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ITUPSAT 1

In orbit NORAD 35935 FMZT-1887-7286-8009-2095 Türkiye

2009

Launch

263

Observations all time

Turkish CubeSat satellite

Mission description

The overall objectives are to provide a hands-on project environment for the students at ITU under faculty guidance. ´The mission goals are to capture imagery of the CMOS payload and to study the behavior of the passive stabilization system of the CubeSat.

Mission information
Spacecraft name
ITUPSAT 1
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
2009-09-23 00:00:00
Separation time
Last observers
Observer
Time of receipt
2026-01-06 08:04:21 UTC
2024-07-21 05:42:34 UTC
2024-07-18 05:14:30 UTC
2023-12-02 19:49:26 UTC
2023-12-02 06:22:11 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
683.90 km
Apogee
692.86 km
Inclination
98.4°
Period
98.6 min
Semi-major axis
7066.5 km
Velocity
7.51 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 14:09:00 UTC
Two-line elements (TLE)
1 35935U 09051E   26286.96431944  .00000786  00000-0  17178-3 0  9992
2 35935 98.3947 195.3098 0006368 224.4938 135.5751 14.60585444906077
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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
2026-10-15 20:30:43 ITUPSAT1
NORAD 35935
FENGYUN 1C DEB
NORAD 30944
4.629 14.78 7.7e-08
2026-10-15 21:00:01 ITUPSAT1
NORAD 35935
FENGYUN 1C DEB
NORAD 36153
1.926 14.74 4.5e-07
2026-10-15 21:25:37 ITUPSAT1
NORAD 35935
SPOT 6
NORAD 38755
2.231 14.57 3.6e-07
2026-10-15 21:27:36 ITUPSAT1
NORAD 35935
DMSP 5D-2 F13 DEB
NORAD 40678
4.232 14.34 1.1e-07
2026-10-16 02:21:41 ITUPSAT1
NORAD 35935
OBJECT C
NORAD 67250
3.548 14.54 1.4e-07
2026-10-16 18:00:57 ITUPSAT1
NORAD 35935
CZ-4B DEB
NORAD 26184
4.383 14.30 1.0e-07
2026-10-17 05:05:33 ITUPSAT1
NORAD 35935
UNKNOWN
NORAD 270066
4.340 11.12 1.7e-07
2026-10-17 19:01:21 ITUPSAT1
NORAD 35935
CZ-6A R/B
NORAD 66051
3.289 14.95 1.4e-07
2026-10-17 20:40:07 ITUPSAT1
NORAD 35935
CZ-6A R/B
NORAD 66051
1.881 14.95 4.3e-07
2026-10-17 22:18:53 ITUPSAT1
NORAD 35935
CZ-6A R/B
NORAD 66051
1.939 14.95 4.0e-07
2026-10-17 23:40:22 ITUPSAT1
NORAD 35935
COSMOS 2251 DEB
NORAD 34270
3.661 13.59 1.7e-07
2026-10-17 23:57:39 ITUPSAT1
NORAD 35935
CZ-6A R/B
NORAD 66051
3.233 14.95 1.4e-07
2026-10-18 01:36:25 ITUPSAT1
NORAD 35935
CZ-6A R/B
NORAD 66051
4.758 14.95 6.7e-08
2026-10-18 22:51:58 ITUPSAT1
NORAD 35935
NOAA 16 DEB
NORAD 41669
4.304 14.08 1.1e-07
2026-10-19 07:51:36 ITUPSAT1
NORAD 35935
COSMOS 2251 DEB
NORAD 34750
4.834 13.54 1.0e-07
2026-10-19 09:23:09 ITUPSAT1
NORAD 35935
DELTA 1 DEB
NORAD 17768
2.812 12.27 3.6e-07
2026-10-19 10:57:43 ITUPSAT1
NORAD 35935
DMSP 5D-2 F13 DEB
NORAD 40517
3.701 14.28 1.4e-07
2026-10-20 06:53:21 ITUPSAT1
NORAD 35935
DELTA 1 DEB
NORAD 42567
2.125 13.23 5.4e-07
2026-10-20 22:38:25 ITUPSAT1
NORAD 35935
CZ-4B DEB
NORAD 26266
3.685 14.66 1.3e-07
2026-10-21 02:02:06 ITUPSAT1
NORAD 35935
CZ-6A R/B
NORAD 66051
4.968 14.97 6.1e-08

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