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 53797U 26145.40453387 +.00000000 +00000-0 +38044-4 0 00009
2 53797 53.2145 289.2995 0001257 82.0958 278.0177 15.08840805 05
| Epoch (UTC): | 25 May 2026 09:42:31 |
| Eccentricity: | 0.0001257 |
| inclination: | 53.2145° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 289.2995° |
| argument of perigee: | 82.0958° |
| revolutions per day: | 15.08840805 |
| mean anomaly at epoch: | 278.0177° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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