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 26039.19723382 +.00000000 +00000-0 -32517-3 0 00004
2 36122 100.3871 355.1881 0007517 164.0825 196.0525 13.16434706 06
| Epoch (UTC): | 08 February 2026 04:44:01 |
| Eccentricity: | 0.0007517 |
| inclination: | 100.3871° |
| perigee height: | 1193 km |
| apogee height: | 1204 km |
| right ascension of ascending node: | 355.1881° |
| argument of perigee: | 164.0825° |
| revolutions per day: | 13.16434706 |
| mean anomaly at epoch: | 196.0525° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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