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 07369U 26150.36203720 +.00000000 +00000-0 +00000-0 0 00005
2 07369 124.8682 239.6522 0066899 72.2922 316.0598 3.07214931 01
| Epoch (UTC): | 30 May 2026 08:41:20 |
| Eccentricity: | 0.0066899 |
| inclination: | 124.8682° |
| perigee height: | 13476 km |
| apogee height: | 13744 km |
| right ascension of ascending node: | 239.6522° |
| argument of perigee: | 72.2922° |
| revolutions per day: | 3.07214931 |
| mean anomaly at epoch: | 316.0598° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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