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VELOX-P 2, 39438

Orbit data source: Space-Track

VELOX-P 2, 39438 is a payload satellite owned by NTU (SG) in SSO that was launched on Thu, 21 Nov 2013 UTC via a DNEPR launch vehicle from the Orenburg, Russia (OREN). 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/39438?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/39438?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

39438, 2013-066Y

Orbit

SSO

Country

SG / SING

Related business

Nanyang Technological University (SG)

Manufacturer

NTU

Mission

Non-operational Amateur Technology

Bus & Motor

CUBESAT 1U, Unknown motor

Mass

1 kg wet, 1 kg dry

Launch date (UTC)

2013-11-21 (12 years ago)

Launch vehicle

DNEPR

Launch site

Orenburg, Russia (OREN)

Object type

Payload

Rocket body

Debris

Shape & HBR

Box, 0.1 m

Radar Cross Section

0.015 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago

0 VELOX-P 2
1 39438U 13066Y   26092.29523914  .00004432  00000-0  42467-3 0  9996
2 39438  97.8687  43.6315 0051885 233.4707 126.1728 14.92666776666514

Epoch: 2026-04-02T07:05Z

TLE epoch observation values (Epoch: 2026-04-02T07:05:08.661Z)

Latitude

-0.0001°

Longitude

106.69966°

Altitude

614.128 km

Speed

7.54 km/s

True Right ascension

02h 54m 31s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

Unknown

Longitude

Unknown

Altitude

Unknown

Speed

Unknown

Apparent Right ascension

Unknown

Apparent Declination

Unknown

Sunlit

N/A

Visualization observer readout

Local Sidereal Time

23:26:28

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

622.784 km

Perigee altitude

550.51 km

Semi-major axis

6,964.784 km

Eccentricity

0.00519

Inclination

97.8687°

RAAN

43.6315°

Arg. of periapsis

233.4707°

True anomaly

126.65092°

Mean anomaly

126.1728°

Eccentric anomaly

126.41204°

Mean motion

3.73406 °/min

Orbital period

96.41 mins

BSTAR

0.00042467

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Other satellites on launch #66 in the year 2013 (2013-11-21 UTC)

DOVE 4, 39434 (Decayed)

BEAKERSAT 1, 39437 (Decayed)

WREN, 39435

QUBESCOUT-S1, 39443 (Decayed)

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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.

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VELOX-P 2 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.
7 mins	2026-04-02 20:05:37.580Z	130.687° SE	2026-04-02 20:08:37.580Z	76.756° E	29.24°	2026-04-02 20:12:37.580Z	6.896° NNE
4 mins	2026-04-02 21:42:37.580Z	235.571° WSW	2026-04-02 21:44:37.580Z	271.176° WNW	18.817°	2026-04-02 21:46:37.580Z	303.716° NW
6 mins	2026-04-03 09:24:37.580Z	22.295° NNE	2026-04-03 09:27:37.580Z	117.55° SE	42.118°	2026-04-03 09:30:37.580Z	181.584° SSW

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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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Check out VELOX-P 2, 39438 on other resources

View VELOX-P 2, 39438 on NASA - NSSDCA Website

View VELOX-P 2, 39438 on Heavens-Above

View VELOX-P 2, 39438 on Keep Track

View VELOX-P 2, 39438 on Celestrak

View VELOX-P 2, 39438 on Gunter's Space Page

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

VELOX-P 2, 39438

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 11 hours ago

TLE from 11 hours ago

TLE epoch observation values (Epoch: 2026-04-02T07:05:08.661Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #66 in the year 2013 (2013-11-21 UTC)

VELOX-P 2 Visibility forecast

Co-orbital & Co-planar RSOs

Check out VELOX-P 2, 39438 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 11 hours ago