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 68552U 26145.32600089 +.00000000 +00000-0 +39265-3 0 00003
2 68552 53.1603 6.2271 0001292 93.1248 266.9902 15.34409612 04
| Epoch (UTC): | 25 May 2026 07:49:26 |
| Eccentricity: | 0.0001292 |
| inclination: | 53.1603° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 6.2271° |
| argument of perigee: | 93.1248° |
| revolutions per day: | 15.34409612 |
| mean anomaly at epoch: | 266.9902° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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