DMSP 5D-2 F14 (USA 131), 24753
Orbit data source: Space-Track
DMSP 5D-2 F14 (USA 131), 24753 is a payload satellite owned by USAF SMC (US) in SSO that was launched on Fri, 04 Apr 1997 UTC via a TITAN II SLV launch vehicle from the Air Force Western Test Range (AFWTR). 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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24753 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
LMT/EW
Mission
Non-operational Defense Weather
Bus & Motor
BLOCK 5D, STAR 37S
Mass
1,456 kg wet, 749 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl + 1 Pan, 6.0 m
Radar Cross Section
4.290 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 DMSP 5D-2 F14 (USA 131)
1 24753U 97012A 26171.42899416 .00000083 00000-0 63221-4 0 9999
2 24753 98.7577 219.9428 0009897 83.9415 276.2887 14.16772915508752Epoch: 2026-06-20T10:17Z
TLE epoch observation values (Epoch: 2026-06-20T10:17:45.095Z)
Latitude
-0.00003°
Longitude
156.86116°
Altitude
838.42 km
Speed
7.434 km/s
True Right ascension
14h 39m 46s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
08:33:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
840.59 km
Perigee altitude
826.315 km
Semi-major axis
7,211.589 km
Eccentricity
0.00099
Inclination
98.7577°
RAAN
219.9428°
Arg. of periapsis
83.9415°
True anomaly
276.17596°
Mean anomaly
276.2887°
Eccentric anomaly
276.23233°
Mean motion
3.54402 °/min
Orbital period
101.58 mins
BSTAR
0.000063221
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Other satellites on launch #12 in the year 1997 (1997-04-04 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.DMSP 5D-2 F14 (USA 131) Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-21 01:43:48.928Z | 88.877° E | 2026-06-21 01:45:48.928Z | 65.728° ENE | 14.429° | 2026-06-21 01:48:48.928Z | 30.315° NE |
| 9 mins | 2026-06-21 03:21:48.928Z | 173.463° S | 2026-06-21 03:25:48.928Z | 239.295° WSW | 43.787° | 2026-06-21 03:30:48.928Z | 342.018° N |
| 8 mins | 2026-06-21 15:42:48.928Z | 33.122° NE | 2026-06-21 15:45:48.928Z | 84.258° E | 36.654° | 2026-06-21 15:50:48.928Z | 172.467° S |
| 6 mins | 2026-06-21 17:23:48.928Z | 330.656° NNW | 2026-06-21 17:25:48.928Z | 303.484° NW | 20.151° | 2026-06-21 17:29:48.928Z | 251.439° W |
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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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