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 27845U 26087.96919206 +.00000000 +00000-0 +23177-3 0 00007
2 27845 98.6665 97.7883 0009805 78.8558 281.3724 14.24879744 00
| Epoch (UTC): | 28 March 2026 23:15:38 |
| Eccentricity: | 0.0009805 |
| inclination: | 98.6665° |
| perigee height: | 802 km |
| apogee height: | 816 km |
| right ascension of ascending node: | 97.7883° |
| argument of perigee: | 78.8558° |
| revolutions per day: | 14.24879744 |
| mean anomaly at epoch: | 281.3724° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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