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 26066.53257417 +.00000000 +00000-0 +72370-3 0 00000
2 40025 98.1011 70.6697 0008059 201.8423 158.2465 15.16462692 03
| Epoch (UTC): | 07 March 2026 12:46:54 |
| Eccentricity: | 0.0008059 |
| inclination: | 98.1011° |
| perigee height: | 511 km |
| apogee height: | 522 km |
| right ascension of ascending node: | 70.6697° |
| argument of perigee: | 201.8423° |
| revolutions per day: | 15.16462692 |
| mean anomaly at epoch: | 158.2465° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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