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 53793U 26145.42664360 +.00000000 +00000-0 +23129-4 0 00000
2 53793 53.2148 289.4300 0001332 102.6519 257.4622 15.08836815 04
| Epoch (UTC): | 25 May 2026 10:14:22 |
| Eccentricity: | 0.0001332 |
| inclination: | 53.2148° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 289.4300° |
| argument of perigee: | 102.6519° |
| revolutions per day: | 15.08836815 |
| mean anomaly at epoch: | 257.4622° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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