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 27640U 26088.00744355 +.00000000 +00000-0 +93835-4 0 00006
2 27640 98.7159 96.1089 0015157 84.5691 275.7214 14.19920213 05
| Epoch (UTC): | 29 March 2026 00:10:43 |
| Eccentricity: | 0.0015157 |
| inclination: | 98.7159° |
| perigee height: | 815 km |
| apogee height: | 837 km |
| right ascension of ascending node: | 96.1089° |
| argument of perigee: | 84.5691° |
| revolutions per day: | 14.19920213 |
| mean anomaly at epoch: | 275.7214° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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