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 26100.90184730 +.00000000 +00000-0 +48954-3 0 00008
2 40025 98.1002 107.3802 0010707 96.5531 263.6920 15.17222184 09
| Epoch (UTC): | 10 April 2026 21:38:39 |
| Eccentricity: | 0.0010707 |
| inclination: | 98.1002° |
| perigee height: | 507 km |
| apogee height: | 522 km |
| right ascension of ascending node: | 107.3802° |
| argument of perigee: | 96.5531° |
| revolutions per day: | 15.17222184 |
| mean anomaly at epoch: | 263.6920° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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