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 27534U 26106.84356176 +.00000000 +00000-0 +49292-4 0 00009
2 27534 82.9394 16.0977 0036904 141.5060 308.0179 13.72956899 04
| Epoch (UTC): | 16 April 2026 20:14:43 |
| Eccentricity: | 0.0036904 |
| inclination: | 82.9394° |
| perigee height: | 962 km |
| apogee height: | 1016 km |
| right ascension of ascending node: | 16.0977° |
| argument of perigee: | 141.5060° |
| revolutions per day: | 13.72956899 |
| mean anomaly at epoch: | 308.0179° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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