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RAPTOR3, 58958

Orbit data source: Space-Track

RAPTOR3, 58958 is a payload satellite owned by SDA (US) in LEO that was launched on Wed, 14 Feb 2024 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

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Identifier
58958, 2024-028D
Orbit
LEO
Last TLE update
9 hours ago
Origin
Manufacturer
L3Harris SIS
Mission
Operational Defense Early Warn
Bus & Motor
TPL0-L3H, Unknown motor
Mass
~1,000 kg wet, ~1,000 kg dry
Launch date (UTC)
2024-02-14 (1 year ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 1 Pan, 2 m
Radar Cross Section
0.945 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 9 hours ago
0 RAPTOR3
1 58958U 24028D   25128.97235912 -.00000021  00000-0  63476-4 0  9991
2 58958  39.9900 100.4558 0010269  84.6887 275.5031 13.70455100 61601
Epoch: 2025-05-08T23:20Z
Definitive object data (Epoch: 2025-05-08T23:20:11.827Z)
Latitude
-0.00003°
Longitude
-116.6287°
Altitude
996.7 km
Speed
7.355 km/s
True Right ascension
06h 41m 49s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at TLE epoch
Visualization TLE readout
Latitude
40.13621°
Longitude
-28.77827°
Altitude
992.668 km
Speed
7.365 km/s
Apparent Right ascension
09h 03m 37s
Apparent Declination
6° 53' 41"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
16:40:13
Azimuth
291.272° WNW
Elevation
-13.561°
Doppler factor
1
Orbital elements
Apogee altitude
1,007.791 km
Perigee altitude
992.638 km
Semi-major axis
7,378.352 km
Eccentricity
0.0010269
Inclination
39.99°
RAAN
100.4558°
Arg. of periapsis
84.6887°
True anomaly
275.38595°
Mean anomaly
275.5031°
Eccentric anomaly
275.44453°
Mean motion
3.42456 °/min
BSTAR
0.000063476
Orbital period
105.12 mins
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Other satellites on launch #28 in the year 2024 (2024-02-14 UTC)

RAPTOR3 Visibility forecast

Observer location: undefined°, undefined°

Span
Click to sort rows by Start time (UTC) header in descending order
Start Az.
Max El. time (UTC)
Max El. Az.
Max El.
End time (UTC)
End Az.
7 mins2025-05-09 08:41:02.765Z253.967° W2025-05-09 08:44:02.765Z223.871° SW17.581°2025-05-09 08:48:02.765Z183.057° SSW
7 mins2025-05-10 00:00:02.765Z173.738° S2025-05-10 00:03:02.765Z139.832° SSE19.736°2025-05-10 00:07:02.765Z99.375° ESE
11 mins2025-05-10 01:48:02.765Z231.771° WSW2025-05-10 01:53:02.765Z165.601° S40.18°2025-05-10 01:59:02.765Z82.018° E
11 mins2025-05-10 03:39:02.765Z265.125° W2025-05-10 03:44:02.765Z265.326° W44.845°2025-05-10 03:50:02.765Z86.997° E
11 mins2025-05-10 05:30:02.765Z277.9° WNW2025-05-10 05:35:02.765Z230.494° WSW43.606°2025-05-10 05:41:02.765Z111.913° ESE
9 mins2025-05-10 07:22:02.765Z264.944° W2025-05-10 07:26:02.765Z214.146° SW29.085°2025-05-10 07:31:02.765Z154.341° SSE
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