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 26032.47959297 +.00000000 +00000-0 +96827-4 0 00003
2 27640 98.7152 41.4247 0013069 241.9402 118.0453 14.19897214 04
| Epoch (UTC): | 01 February 2026 11:30:36 |
| Eccentricity: | 0.0013069 |
| inclination: | 98.7152° |
| perigee height: | 816 km |
| apogee height: | 835 km |
| right ascension of ascending node: | 41.4247° |
| argument of perigee: | 241.9402° |
| revolutions per day: | 14.19897214 |
| mean anomaly at epoch: | 118.0453° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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