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 27057U 26159.44651116 +.00000000 +00000-0 -31923-4 0 00008
2 27057 82.5441 219.7599 0001648 99.8472 260.2805 12.61616582 08
| Epoch (UTC): | 08 June 2026 10:42:58 |
| Eccentricity: | 0.0001648 |
| inclination: | 82.5441° |
| perigee height: | 1415 km |
| apogee height: | 1418 km |
| right ascension of ascending node: | 219.7599° |
| argument of perigee: | 99.8472° |
| revolutions per day: | 12.61616582 |
| mean anomaly at epoch: | 260.2805° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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