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 40025U 26072.47086215 +.00000000 +00000-0 +58762-3 0 00005
2 40025 98.1008 77.0094 0008779 180.8547 179.2670 15.16608356 03
| Epoch (UTC): | 13 March 2026 11:18:02 |
| Eccentricity: | 0.0008779 |
| inclination: | 98.1008° |
| perigee height: | 510 km |
| apogee height: | 522 km |
| right ascension of ascending node: | 77.0094° |
| argument of perigee: | 180.8547° |
| revolutions per day: | 15.16608356 |
| mean anomaly at epoch: | 179.2670° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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