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 36122U 26145.52014512 +.00000000 +00000-0 +47473-3 0 00003
2 36122 100.4014 99.7159 0006871 288.1470 71.8894 13.16439746 09
| Epoch (UTC): | 25 May 2026 12:29:00 |
| Eccentricity: | 0.0006871 |
| inclination: | 100.4014° |
| perigee height: | 1193 km |
| apogee height: | 1204 km |
| right ascension of ascending node: | 99.7159° |
| argument of perigee: | 288.1470° |
| revolutions per day: | 13.16439746 |
| mean anomaly at epoch: | 71.8894° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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