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 52627U 26145.35536778 +.00000000 +00000-0 +47907-4 0 00008
2 52627 53.2136 284.9530 0001187 99.6519 260.4607 15.08838365 03
| Epoch (UTC): | 25 May 2026 08:31:43 |
| Eccentricity: | 0.0001187 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 284.9530° |
| argument of perigee: | 99.6519° |
| revolutions per day: | 15.08838365 |
| mean anomaly at epoch: | 260.4607° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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