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 39077U 26145.58171100 +.00000000 +00000-0 +89951-4 0 00006
2 39077 52.0099 350.0215 0000463 107.0645 253.0273 12.62263043 06
| Epoch (UTC): | 25 May 2026 13:57:39 |
| Eccentricity: | 0.0000463 |
| inclination: | 52.0099° |
| perigee height: | 1413 km |
| apogee height: | 1414 km |
| right ascension of ascending node: | 350.0215° |
| argument of perigee: | 107.0645° |
| revolutions per day: | 12.62263043 |
| mean anomaly at epoch: | 253.0273° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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