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 49077U 26145.08204517 +.00000000 +00000-0 +13488-3 0 00002
2 49077 87.9153 10.4610 0002122 93.1233 267.0141 13.17651496 06
| Epoch (UTC): | 25 May 2026 01:58:08 |
| Eccentricity: | 0.0002122 |
| inclination: | 87.9153° |
| perigee height: | 1192 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 10.4610° |
| argument of perigee: | 93.1233° |
| revolutions per day: | 13.17651496 |
| mean anomaly at epoch: | 267.0141° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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