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 53853U 26145.44687105 +.00000000 +00000-0 +53236-4 0 00003
2 53853 53.2118 309.2402 0001288 88.0715 272.0425 15.08840636 07
| Epoch (UTC): | 25 May 2026 10:43:29 |
| Eccentricity: | 0.0001288 |
| inclination: | 53.2118° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 309.2402° |
| argument of perigee: | 88.0715° |
| revolutions per day: | 15.08840636 |
| mean anomaly at epoch: | 272.0425° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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