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 22287U 26067.27594604 +.00000000 +00000-0 +83928-4 0 00006
2 22287 82.5276 354.1811 0023419 344.7809 15.2696 14.80050399 08
| Epoch (UTC): | 08 March 2026 06:37:21 |
| Eccentricity: | 0.0023419 |
| inclination: | 82.5276° |
| perigee height: | 613 km |
| apogee height: | 646 km |
| right ascension of ascending node: | 354.1811° |
| argument of perigee: | 344.7809° |
| revolutions per day: | 14.80050399 |
| mean anomaly at epoch: | 15.2696° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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