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 27819U 26064.77136178 +.00000000 +00000-0 +12613-3 0 00004
2 27819 82.9510 190.8570 0046395 189.3271 281.4567 13.74535057 05
| Epoch (UTC): | 05 March 2026 18:30:45 |
| Eccentricity: | 0.0046395 |
| inclination: | 82.9510° |
| perigee height: | 949 km |
| apogee height: | 1017 km |
| right ascension of ascending node: | 190.8570° |
| argument of perigee: | 189.3271° |
| revolutions per day: | 13.74535057 |
| mean anomaly at epoch: | 281.4567° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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