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 22639U 26087.90673661 +.00000000 +00000-0 +69542-4 0 00006
2 22639 69.9198 165.2892 0065849 301.9297 57.5433 14.32955246 00
| Epoch (UTC): | 28 March 2026 21:45:42 |
| Eccentricity: | 0.0065849 |
| inclination: | 69.9198° |
| perigee height: | 735 km |
| apogee height: | 829 km |
| right ascension of ascending node: | 165.2892° |
| argument of perigee: | 301.9297° |
| revolutions per day: | 14.32955246 |
| mean anomaly at epoch: | 57.5433° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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