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 53027U 26145.28591080 +.00000000 +00000-0 +33209-3 0 00001
2 53027 53.2137 100.2651 0001483 80.7728 279.3432 15.08813161 07
| Epoch (UTC): | 25 May 2026 06:51:42 |
| Eccentricity: | 0.0001483 |
| inclination: | 53.2137° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 100.2651° |
| argument of perigee: | 80.7728° |
| revolutions per day: | 15.08813161 |
| mean anomaly at epoch: | 279.3432° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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