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 53020U 26145.13134824 +.00000000 +00000-0 +31396-4 0 00003
2 53020 53.2148 100.9581 0001333 75.3057 284.8082 15.08840217 04
| Epoch (UTC): | 25 May 2026 03:09:08 |
| Eccentricity: | 0.0001333 |
| inclination: | 53.2148° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 100.9581° |
| argument of perigee: | 75.3057° |
| revolutions per day: | 15.08840217 |
| mean anomaly at epoch: | 284.8082° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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