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 26144.94814720 +.00000000 +00000-0 +36516-3 0 00000
2 40025 98.0976 154.4718 0007249 313.3224 46.7403 15.17843028 05
| Epoch (UTC): | 24 May 2026 22:45:19 |
| Eccentricity: | 0.0007249 |
| inclination: | 98.0976° |
| perigee height: | 507 km |
| apogee height: | 517 km |
| right ascension of ascending node: | 154.4718° |
| argument of perigee: | 313.3224° |
| revolutions per day: | 15.17843028 |
| mean anomaly at epoch: | 46.7403° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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