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 22824U 26088.21522925 +.00000000 +00000-0 +65338-5 0 00003
2 22824 98.7800 152.1527 0007431 107.2272 315.2515 14.27468143 03
| Epoch (UTC): | 29 March 2026 05:09:55 |
| Eccentricity: | 0.0007431 |
| inclination: | 98.7800° |
| perigee height: | 795 km |
| apogee height: | 806 km |
| right ascension of ascending node: | 152.1527° |
| argument of perigee: | 107.2272° |
| revolutions per day: | 14.27468143 |
| mean anomaly at epoch: | 315.2515° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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