MORELOS 2 R/B(PAM-D), 16293
Orbit data source: Space-Track
MORELOS 2 R/B(PAM-D), 16293 is space debris in HEO originally from a launch on Wed, 27 Nov 1985 UTC launched from the Air Force Eastern Test Range (AFETR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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16293 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Thiokol/TE
Mission
Spacecraft
Bus & Motor
STAR 48, Unknown motor
Mass
132 kg wet, 132 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 MORELOS 2 R/B(PAM-D)
1 16293U 85109F 25341.07798074 .00000251 00000-0 86073-3 0 9996
2 16293 25.7065 254.7741 7137962 295.1458 9.4160 2.37645994276214Epoch: 2025-12-07T01:52Z
TLE epoch observation values (Epoch: 2025-12-07T01:52:17.535Z)
Latitude
0.00003°
Longitude
150.6186°
Altitude
2,564.963 km
Speed
8.505 km/s
True Right ascension
16h 59m 09s
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
22:44:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
34,279.798 km
Perigee altitude
411.734 km
Semi-major axis
23,723.903 km
Eccentricity
0.7138
Inclination
25.7065°
RAAN
254.7741°
Arg. of periapsis
295.1458°
True anomaly
65.85097°
Mean anomaly
9.416°
Eccentric anomaly
29.64478°
Mean motion
0.59397 °/min
Orbital period
606.09 mins
BSTAR
0.00086073
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Other satellites on launch #109 in the year 1985 (1985-11-27 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.MORELOS 2 R/B(PAM-D) 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. |
|---|---|---|---|---|---|---|---|
| 407 mins | 2025-12-08 00:36:58.349Z | 151.226° SSE | 2025-12-08 01:45:58.349Z | 166.529° S | 43.459° | 2025-12-08 07:23:58.349Z | 167.953° S |
| 377 mins | 2025-12-08 18:19:58.349Z | 151.903° SSE | 2025-12-09 00:36:58.349Z | 104.445° ESE | 31.985° | 2025-12-09 00:36:58.349Z | 104.445° ESE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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