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 52834U 26145.46715007 +.00000000 +00000-0 +54257-4 0 00000
2 52834 53.2136 49.4507 0001358 88.0746 272.0402 15.08834683 06
| Epoch (UTC): | 25 May 2026 11:12:41 |
| Eccentricity: | 0.0001358 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 49.4507° |
| argument of perigee: | 88.0746° |
| revolutions per day: | 15.08834683 |
| mean anomaly at epoch: | 272.0402° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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