View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 00205U 26149.53843404 +.00000000 +00000-0 +55291-4 0 00009
2 00205 32.4406 251.4821 0101871 191.4874 168.3415 13.62572866 07
| Epoch (UTC): | 29 May 2026 12:55:20 |
| Eccentricity: | 0.0101871 |
| inclination: | 32.4406° |
| perigee height: | 951 km |
| apogee height: | 1102 km |
| right ascension of ascending node: | 251.4821° |
| argument of perigee: | 191.4874° |
| revolutions per day: | 13.62572866 |
| mean anomaly at epoch: | 168.3415° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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