PSN N5, 65588
Orbit data source: Space-Track
PSN N5, 65588 is a payload satellite owned by SNT (ID) in HEO that was launched on Fri, 12 Sep 2025 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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65588 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / INDORelated business
None
Manufacturer
Boeing/ES
Mission
Operational spacecraft
Bus & Motor
BSS-702MP, R-4D?
Mass
7,800 kg wet, ~4,500 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 6 days ago
TLE from 6 days ago
0 PSN N5
1 65588U 25205A 25255.10218750 .00000041 00000-0 00000-0 0 9994
2 65588 26.4759 204.2219 5387164 174.0939 9.9928 5.04113332 14Epoch: 2025-09-12T02:27Z
TLE epoch observation values (Epoch: 2025-09-12T02:27:08.999Z)
Latitude
-13.69986°
Longitude
25.17197°
Altitude
773.778 km
Speed
9.151 km/s
True Right ascension
03h 33m 15s
True Declination
-13° 37' 16"
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
12:36:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
15,735.016 km
Perigee altitude
251.047 km
Semi-major axis
14,371.168 km
Eccentricity
0.53872
Inclination
26.4759°
RAAN
204.2219°
Arg. of periapsis
174.0939°
True anomaly
37.58705°
Mean anomaly
9.9928°
Eccentric anomaly
21.1091°
Mean motion
1.25981 °/min
Orbital period
285.76 mins
BSTAR
0
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Other satellites on launch #205 in the year 2025 (2025-09-12 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.PSN N5 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. |
|---|---|---|---|---|---|---|---|
| 172 mins | 2025-09-17 21:55:57.710Z | 227.098° WSW | 2025-09-18 00:23:57.710Z | 174.867° S | 41.152° | 2025-09-18 00:47:57.710Z | 101.144° ESE |
| 21 mins | 2025-09-18 05:22:57.710Z | 269.746° W | 2025-09-18 05:37:57.710Z | 231.937° WSW | 21.245° | 2025-09-18 05:43:57.710Z | 180.386° SSW |
| 154 mins | 2025-09-18 16:35:57.710Z | 149.713° SSE | 2025-09-18 18:10:57.710Z | 116.017° SE | 20.126° | 2025-09-18 19:09:57.710Z | 90.337° ESE |
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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