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 22488U 26075.89109693 +.00000000 +00000-0 -92625-5 0 00002
2 22488 82.9422 220.6371 0024020 270.7974 254.4928 13.77994752 06
| Epoch (UTC): | 16 March 2026 21:23:10 |
| Eccentricity: | 0.0024020 |
| inclination: | 82.9422° |
| perigee height: | 953 km |
| apogee height: | 989 km |
| right ascension of ascending node: | 220.6371° |
| argument of perigee: | 270.7974° |
| revolutions per day: | 13.77994752 |
| mean anomaly at epoch: | 254.4928° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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