IKONOS 2 (25919)

COSPAR: 1999-051A | Alt Name: Ikonos

Image
IKONOS 2 Satellite Image
Additional Sources
Launch Details

Launch Date

September 24, 1999

Launch Site

AFWTR

Launch Pad

SLC6

Launch Vehicle

Athena-2

Orbital Elements

NORAD ID

25919

International Designator

1999-051A

Epoch

Sat, 04 Jul 2026 01:27:31 GMT

Apogee

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Perigee

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Inclination

98.13°

Right Ascension

74.65°

Eccentricity

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Argument of Perigee

134.81°

Period

96.17 min

Mean Motion

14.97 rev/day

Latitude

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Longitude

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Altitude

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Velocity

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Polar Plot
3D Visualization
Basic Satellite Info

Name

IKONOS 2

Alternative Name

Ikonos

Type

Payload

Status

Non-operational

Owner

SIMG

Country

United States

Constellation

N/A

Related Satellites

Major Events

N/A

Latest TLEs
1 25919U 99051A   26185.06077915  .00001918  00000-0  17040-3 0  9991
2 25919  98.1329  74.6481 0006984 134.8143 225.3646 14.97409327441442

Source: Celestrak

Summary
IKONOS 2, also known as Ikonos, is an Earth observation satellite with NORAD identifier 25919 and OBJECT_ID 1999-051A. Launched on September 24, 1999, from the AFWTR SLC6 pad using the Athena-2 launch vehicle, this US-built spacecraft was manufactured by LMMS (Lockheed Martin Missiles and Space). The satellite has a box-like shape with a pan extension, measuring approximately 2 meters in length and diameter of 1.5 meters. It weighs 726 kilograms at launch and 688 kilograms dry. IKONOS 2 is equipped with three deployable fixed solar arrays and batteries for power generation. Its mission is to conduct Earth observation with a design lifetime of 7 years, though it achieved an operational lifespan of 15 years. The satellite has an RCS (Reflective Cross Section) value of 3.873. Owned by SIMG (Space Imaging), IKONOS 2's payload consists of its namesake imaging system designed for high-resolution Earth observation.
Physical Characteristics

Length

2

Diameter

1.5

Span

2

Dry Mass

688

Launch Mass

726

Shape

Box + Pan

Radar Cross Section

3.873

Visual Magnitude

Unknown

Color

Unknown

Material Composition

Unknown

Technical Details

Payload

Ikonos 2

Purpose

Earth observation

Mission

Earth observation

Manufacturer

LMMS

Life Expectancy

7 years (design); 15 years (achieved)

Bus

LM-900

Configuration

LM-900

Motor

Unknown

Equipment

Unknown

Power System

3 deployable fixed solar arrays, batteries

ADCS

Unknown

Transmitter Frequency

Unknown

Map
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