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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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<iframe src="https://www.satcat.com/sats-embedded/1510?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/1510?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

1510, 1965-065C

Orbit

LEO

Last TLE update

7 hours ago

Origin

United States Navy (US)

Manufacturer

NRL

Mission

Defense Calibration

Bus & Motor

NRL 9", Unknown motor

Mass

4 kg wet, 4 kg dry

Launch date (UTC)

1965-08-13 (60 years ago)

Launch vehicle

THOR ABLESTAR

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Sphere + 12 Rod, 15.2 m

Radar Cross Section

0.071 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 7 hours ago

0 DODECAPOLE 2
1 01510U 65065C   25182.84424031  .00002766  00000-0  16059-2 0  9997
2 01510  90.0565  22.6020 0034837 220.0682 139.7931 14.08233710983812

Epoch: 2025-07-01T20:15Z

TLE epoch observation values (Epoch: 2025-07-01T20:15:42.362Z)

Latitude

-0.0001°

Longitude

158.54163°

Altitude

887.773 km

Speed

7.398 km/s

True Right ascension

01h 30m 24s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

70.30236°

Longitude

158.38651°

Altitude

899.253 km

Speed

7.398 km/s

Apparent Right ascension

02h 34m 14s

Apparent Declination

20° 55' 32"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

15:06:17

Azimuth

8.533° NNE

Elevation

-28.701°

Doppler factor

Orbital elements

Apogee altitude

887.611 km

Perigee altitude

837.164 km

Semi-major axis

7,240.525 km

Eccentricity

0.00348

Inclination

90.0565°

RAAN

22.602°

Arg. of periapsis

220.0682°

True anomaly

Unknown

Mean anomaly

139.7931°

Eccentric anomaly

Unknown

Mean motion

3.5228 °/min

Orbital period

102.19 mins

BSTAR

0.0016059

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Other satellites on launch #65 in the year 1965 (1965-08-13 UTC)

THOR ABLESTAR DEB, 1504

THOR ABLESTAR R/B, 1508

THOR ABLESTAR DEB, 1511

TEMPSAT 1, 1512

OPS 8464 (TRANSIT 5B-7), 1514

NAVSPASUR ROD 1, 1515

CALSPHERE 4(A), 1520

PORCUPINE 2, 1577

THOR ABLESTAR DEB, 1521

THOR ABLESTAR DEB, 1522

OPS 8464 DEB *, 2335 (Decayed)

TRANSIT 5B-7 DEB, 3809 (Decayed)

THOR ABLESTAR DEB, 3810

THOR ABLESTAR DEB, 5265

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.
10 mins	2025-07-02 13:25:02.751Z	163.771° S	2025-07-02 13:30:02.751Z	103.242° ESE	41.832°	2025-07-02 13:35:02.751Z	5.822° NNE
5 mins	2025-07-02 15:11:02.751Z	258.429° W	2025-07-02 15:13:02.751Z	282.261° WNW	15.682°	2025-07-02 15:16:02.751Z	315.414° NNW
9 mins	2025-07-03 01:51:02.751Z	356.918° N	2025-07-03 01:55:02.751Z	277.732° WNW	44.021°	2025-07-03 02:00:02.751Z	191.054° SSW

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Check out DODECAPOLE 2, 1510 on other resources

View DODECAPOLE 2, 1510 on NASA - NSSDCA Website

View DODECAPOLE 2, 1510 on Heavens-Above

View DODECAPOLE 2, 1510 on Keep Track

View DODECAPOLE 2, 1510 on Celestrak

View DODECAPOLE 2, 1510 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.