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 53918U 26145.51128828 +.00000000 +00000-0 +14929-5 0 00002
2 53918 53.2151 329.1587 0001422 93.1169 266.9986 15.08839693 06
| Epoch (UTC): | 25 May 2026 12:16:15 |
| Eccentricity: | 0.0001422 |
| inclination: | 53.2151° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 329.1587° |
| argument of perigee: | 93.1169° |
| revolutions per day: | 15.08839693 |
| mean anomaly at epoch: | 266.9986° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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