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 27842U 26068.59694817 +.00000000 +00000-0 +16877-3 0 00009
2 27842 98.6891 78.2379 0010410 91.7744 268.4627 14.23873634 06
| Epoch (UTC): | 09 March 2026 14:19:36 |
| Eccentricity: | 0.0010410 |
| inclination: | 98.6891° |
| perigee height: | 805 km |
| apogee height: | 820 km |
| right ascension of ascending node: | 78.2379° |
| argument of perigee: | 91.7744° |
| revolutions per day: | 14.23873634 |
| mean anomaly at epoch: | 268.4627° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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