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CUBESAT XI 4, 27848

Orbit data source: Space-Track

CUBESAT XI 4, 27848 is a payload satellite owned by Tokyo (JP) in SSO that was launched on Mon, 30 Jun 2003 UTC via an ROKOT launch vehicle from the Plesetsk Missile And Space Complex (PKMTR). 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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https://www.satcat.com/sats-embedded/27848?theme=dark&initialShowStats=false

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Identifier

27848, 2003-031J

Orbit

SSO

Last TLE update

1 day ago

Origin

The University of Tokyo (JP / JPN)

Manufacturer

Tokyo

Mission

Operational Amateur Technology

Bus & Motor

CUBESAT 1U, Unknown motor

Mass

1 kg wet, 1 kg dry

Launch date (UTC)

2003-06-30 (22 years ago)

Launch vehicle

ROKOT

Launch site

Plesetsk Missile And Space Complex (PKMTR)

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

TLE from 1 day ago

0 CUBESAT XI 4
1 27848U 03031J   25170.54016859  .00000226  00000-0  11891-3 0  9992
2 27848  98.6781 178.6830 0009710 168.6411 191.4989 14.23337433139835

Epoch: 2025-06-19T12:57Z

TLE epoch observation values (Epoch: 2025-06-19T12:57:50.566Z)

Latitude

0.00006°

Longitude

76.21591°

Altitude

823.853 km

Speed

7.438 km/s

True Right ascension

11h 54m 43s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

37.04147°

Longitude

70.68336°

Altitude

823.444 km

Speed

7.443 km/s

Apparent Right ascension

12h 23m 03s

Apparent Declination

1° 21' 47"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

01:22:31

Azimuth

21.892° NNE

Elevation

-46.539°

Doppler factor

Orbital elements

Apogee altitude

818.221 km

Perigee altitude

804.26 km

Semi-major axis

7,189.378 km

Eccentricity

0.00097

Inclination

98.6781°

RAAN

178.683°

Arg. of periapsis

168.6411°

True anomaly

Unknown

Mean anomaly

191.4989°

Eccentric anomaly

Unknown

Mean motion

3.56046 °/min

Orbital period

101.11 mins

BSTAR

0.00011891

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Other satellites on launch #31 in the year 2003 (2003-06-30 UTC)

MONITOR-E/SL-19, 27840

MIMOSA, 27841 (Decayed)

CUBESAT XI 4 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.
6 mins	2025-06-20 14:50:46.904Z	335.471° NNW	2025-06-20 14:53:46.904Z	299.484° NW	16.477°	2025-06-20 14:56:46.904Z	262.391° W
9 mins	2025-06-21 00:30:46.904Z	165.984° S	2025-06-21 00:34:46.904Z	181.57° SSW	44.813°	2025-06-21 00:39:46.904Z	346.039° N
7 mins	2025-06-21 12:48:46.904Z	42.055° NE	2025-06-21 12:51:46.904Z	95.995° ESE	31.386°	2025-06-21 12:55:46.904Z	160.387° S

Authenticating...

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Check out CUBESAT XI 4, 27848 on other resources

View CUBESAT XI 4, 27848 on NASA - NSSDCA Website

View CUBESAT XI 4, 27848 on Heavens-Above

View CUBESAT XI 4, 27848 on Keep Track

View CUBESAT XI 4, 27848 on Celestrak

View CUBESAT XI 4, 27848 on Gunter's Space Page

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