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 26088.16631332 +.00000000 +00000-0 +51099-4 0 00001
2 22287 82.5257 334.7313 0022265 272.9119 86.9547 14.80067221 04
| Epoch (UTC): | 29 March 2026 03:59:29 |
| Eccentricity: | 0.0022265 |
| inclination: | 82.5257° |
| perigee height: | 614 km |
| apogee height: | 645 km |
| right ascension of ascending node: | 334.7313° |
| argument of perigee: | 272.9119° |
| revolutions per day: | 14.80067221 |
| mean anomaly at epoch: | 86.9547° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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