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 22877U 26121.39784213 +.00000000 +00000-0 +00000-0 0 00008
2 22877 55.4498 338.9381 0008164 128.4127 55.1503 1.88541243 07
| Epoch (UTC): | 01 May 2026 09:32:53 |
| Eccentricity: | 0.0008164 |
| inclination: | 55.4498° |
| perigee height: | 21277 km |
| apogee height: | 21322 km |
| right ascension of ascending node: | 338.9381° |
| argument of perigee: | 128.4127° |
| revolutions per day: | 1.88541243 |
| mean anomaly at epoch: | 55.1503° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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