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 22087U 26149.91807323 +.00000000 +00000-0 +00000-0 0 00007
2 22087 12.9158 24.2548 0007870 113.8156 137.2213 0.99201773 06
| Epoch (UTC): | 29 May 2026 22:02:01 |
| Eccentricity: | 0.0007870 |
| inclination: | 12.9158° |
| perigee height: | 36056 km |
| apogee height: | 36123 km |
| right ascension of ascending node: | 24.2548° |
| argument of perigee: | 113.8156° |
| revolutions per day: | 0.99201773 |
| mean anomaly at epoch: | 137.2213° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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