DODECAPOLE 2, 1510
Orbit data source: Space-Track
DODECAPOLE 2, 1510 is a payload satellite owned by NRL (US) in LEO that was launched on Fri, 13 Aug 1965 UTC via a THOR ABLESTAR 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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1510 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
NRL
Mission
Defense Calibration
Bus & Motor
NRL 9", Unknown motor
Mass
4 kg wet, 4 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Sphere + 12 Rod, 7.6 m
Radar Cross Section
0.071 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 DODECAPOLE 2
1 01510U 65065C 25242.87890219 .00005378 00000-0 31037-2 0 9997
2 01510 90.0600 22.9789 0036859 35.9929 324.3727 14.08603372992269Epoch: 2025-08-30T21:05Z
TLE epoch observation values (Epoch: 2025-08-30T21:05:37.149Z)
Latitude
0.00007°
Longitude
87.26724°
Altitude
845.525 km
Speed
7.441 km/s
True Right ascension
01h 31m 54s
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
18:55:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
887.803 km
Perigee altitude
834.436 km
Semi-major axis
7,239.257 km
Eccentricity
0.00369
Inclination
90.06°
RAAN
22.9789°
Arg. of periapsis
35.9929°
True anomaly
324.12574°
Mean anomaly
324.3727°
Eccentric anomaly
324.24931°
Mean motion
3.52373 °/min
Orbital period
102.16 mins
BSTAR
0.0031037
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Other satellites on launch #65 in the year 1965 (1965-08-13 UTC)
DODECAPOLE 2 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-08-31 09:08:31.786Z | 145.512° SSE | 2025-08-31 09:13:31.786Z | 70.034° E | 31.847° | 2025-08-31 09:17:31.786Z | 16.504° NNE |
| 7 mins | 2025-08-31 10:52:31.786Z | 236.829° WSW | 2025-08-31 10:55:31.786Z | 280.84° WNW | 22.478° | 2025-08-31 10:59:31.786Z | 329.706° NNW |
| 9 mins | 2025-08-31 21:33:31.786Z | 11.491° NNE | 2025-08-31 21:37:31.786Z | 105.373° ESE | 42.809° | 2025-08-31 21:42:31.786Z | 173.582° S |
| 4 mins | 2025-08-31 23:17:31.786Z | 302.129° NW | 2025-08-31 23:18:31.786Z | 290.149° WNW | 14.733° | 2025-08-31 23:21:31.786Z | 256.6° 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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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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Authenticating...
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