ANALYST OBJECT, 89496

Orbit data source: Space-Track

You're viewing an Uncataloged Satellite

Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, Bus, Motor, and Mission.

Analyst objects are objects on Earth’s orbit with insufficient fidelity to be published in the public satellite catalog. This can be due to infrequent tracking, cross-tagging (observation association with closely-spaced objects), or inability to associate the object with a known launch.

Not visible in the next 10 days

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https://www.satcat.com/sats-embedded/89496?theme=dark&initialShowStats=false

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ISO8601 Format

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ISO8601 Format

Identifier

89496

Orbit

SSO

Last TLE update

3 years ago

Origin

Unknown

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

Unknown

Launch vehicle

Unknown

Launch site

Unknown

Object type

Unknown

Shape & HBR

Unknown

Radar Cross Section

RCS unknown

Expand to show TLE details & history

TLE from 3 years ago

TBA - TO BE ASSIGNED
1 89496U          23012.06387927 +.00110967 +00000+0 +77979-2 0  9990
2 89496  98.8528 117.6244 0056777 140.0954 220.4463 15.03274294321743

Epoch: 2023-01-12T01:31Z

TLE epoch observation values (Epoch: 2023-01-12T01:31:59.168Z)

Latitude

-0.00001°

Longitude

-16.66855°

Altitude

589.895 km

Speed

7.549 km/s

True Right ascension

07h 50m 29s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization observer readout

Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.

Visualization observer readout

Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed.

Orbital elements

Apogee altitude

593.221 km

Perigee altitude

514.506 km

Semi-major axis

6,932 km

Eccentricity

0.00568

Inclination

98.8528°

RAAN

117.6244°

Arg. of periapsis

140.0954°

True anomaly

Unknown

Mean anomaly

220.4463°

Eccentric anomaly

Unknown

Mean motion

3.76058 °/min

Orbital period

95.73 mins

BSTAR

0.0077979

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Other satellites on launch

Visibility

Observer location: undefined°, undefined°

This satellite is likely not visible in the next few days

Co-orbital & Co-planar RSOs

Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions

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Check out ANALYST OBJECT, 89496 on other resources

View ANALYST OBJECT, 89496 on Celestrak

View ANALYST OBJECT, 89496 on Gunter's Space Page

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