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CUBESAT XI-IV

In orbit NORAD 27848 KZUI-4275-4790-4963-1514 Japan

2003

Launch

310

Observations all time

Japanese CubeSat

Mission description

The objective is to demonstrate and to validate a picosatellite bus system and the space use of commercial-of-the-shelf (COTS) parts. CMOS camera.

Mission information
Spacecraft name
CUBESAT XI-IV
Other names
CO-57
Mass
1.0 kg
Form factor
1U
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Launch time
2003-06-30 00:00:00
Separation time
Last observers
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
803.96 km
Apogee
816.29 km
Inclination
98.7°
Period
101.1 min
Semi-major axis
7188.3 km
Velocity
7.44 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 12:56:42 UTC
Two-line elements (TLE)
1 27848U 03031J   26284.27184076  .00000205  00000-0  10916-3 0  9990
2 27848 98.6800 291.0124 0008649 222.7572 137.2935 14.23670205207891
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Orbit history, past year

Mean elements of every TLE set over the past 365 days, plotted against the epoch of the set. Each source is its own line; click it in the legend to hide it. A jump in altitude is a manoeuvre or a bad set; lines drifting apart are a disagreement between sources. “TLE age” is how many hours have passed since the epoch of the source's freshest set, plotted against when the set reached us, on a logarithmic scale. A set the source repeats unchanged does not reset the age.

Prediction divergence

Each TLE set is propagated with SGP4 to the epoch of the next set from the same source and compared with it, plotted against the epoch of the next set; the tooltip shows how many hours ahead the prediction ran. The logarithmic scale shows the size of the divergence and the tooltip its sign: plus along-track means the prediction is ahead of the satellite. This is how well the sets agree, not the true error: the reference is a TLE too, off by about a kilometre. An outlier is a manoeuvre between sets. Sets more than a week apart are not compared.

Time of closest approach, UTC Object 1 Object 2 Distance, km Speed, km/s Max. probability
2026-10-12 20:49:50 CUBESAT XI-IV (CO-57)
NORAD 27848
FENGYUN 1C DEB
NORAD 31760
2.400 12.42 4.7e-07
2026-10-13 17:37:04 CUBESAT XI-IV (CO-57)
NORAD 27848
CZ-6A DEB
NORAD 54491
4.431 0.07 2.1e-07
2026-10-13 17:46:00 CUBESAT XI-IV (CO-57)
NORAD 27848
THOR BURNER 2 R/B
NORAD 3271
3.999 14.57 7.1e-08
2026-10-13 20:16:04 CUBESAT XI-IV (CO-57)
NORAD 27848
FENGYUN 1C DEB
NORAD 32160
4.033 14.58 1.0e-07
2026-10-14 04:37:15 CUBESAT XI-IV (CO-57)
NORAD 27848
NOAA 11 DEB
NORAD 37241
4.376 14.69 8.5e-08
2026-10-14 05:47:42 CUBESAT XI-IV (CO-57)
NORAD 27848
FENGYUN 1C DEB
NORAD 30949
4.255 1.93 2.4e-07
2026-10-14 13:22:01 CUBESAT XI-IV (CO-57)
NORAD 27848
NOAA 16 DEB
NORAD 41206
3.813 4.17 2.9e-07
2026-10-14 16:45:24 CUBESAT XI-IV (CO-57)
NORAD 27848
CZ-6A DEB
NORAD 54360
3.505 1.49 3.6e-07
2026-10-14 20:56:59 CUBESAT XI-IV (CO-57)
NORAD 27848
FENGYUN 1C DEB
NORAD 32086
4.951 5.31 1.7e-07
2026-10-15 00:46:22 CUBESAT XI-IV (CO-57)
NORAD 27848
OPS 7869 (DMSP 4B F1)
NORAD 3266
2.678 14.74 2.4e-07
2026-10-15 14:49:32 CUBESAT XI-IV (CO-57)
NORAD 27848
THOR ABLESTAR DEB
NORAD 324
3.076 14.34 2.0e-07
2026-10-15 22:15:19 CUBESAT XI-IV (CO-57)
NORAD 27848
METOP-B
NORAD 38771
3.526 5.31 3.3e-07
2026-10-16 00:53:33 CUBESAT XI-IV (CO-57)
NORAD 27848
CZ-6A DEB
NORAD 63921
2.380 14.76 2.7e-07
2026-10-16 16:04:38 CUBESAT XI-IV (CO-57)
NORAD 27848
THORAD AGENA D DEB
NORAD 4180
4.084 10.32 2.0e-07
2026-10-16 21:54:57 CUBESAT XI-IV (CO-57)
NORAD 27848
UNKNOWN
NORAD 81844
3.939 10.86 2.1e-07
2026-10-17 04:46:20 CUBESAT XI-IV (CO-57)
NORAD 27848
FENGYUN 1C DEB
NORAD 37406
4.506 14.30 9.3e-08
2026-10-17 06:18:26 CUBESAT XI-IV (CO-57)
NORAD 27848
DELTA 1 DEB
NORAD 37662
4.219 2.10 2.5e-07

Data: CelesTrak SOCRATES Plus, computed from TLEs of the public catalog. This is an estimate, not grounds for a manoeuvre: TLEs carry no covariance, and the maximum probability assumes a position error.

All conjunctions of this satellite