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 26053.73482161 +.00000000 +00000-0 +43291-4 0 00005
2 27534 82.9318 55.3440 0034823 291.8622 248.1532 13.72951605 09
| Epoch (UTC): | 22 February 2026 17:38:08 |
| Eccentricity: | 0.0034823 |
| inclination: | 82.9318° |
| perigee height: | 963 km |
| apogee height: | 1015 km |
| right ascension of ascending node: | 55.3440° |
| argument of perigee: | 291.8622° |
| revolutions per day: | 13.72951605 |
| mean anomaly at epoch: | 248.1532° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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