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 26087.84226631 +.00000000 +00000-0 +57652-3 0 00007
2 40025 98.1001 93.4257 0010265 133.3453 226.8635 15.16904902 07
| Epoch (UTC): | 28 March 2026 20:12:51 |
| Eccentricity: | 0.0010265 |
| inclination: | 98.1001° |
| perigee height: | 508 km |
| apogee height: | 522 km |
| right ascension of ascending node: | 93.4257° |
| argument of perigee: | 133.3453° |
| revolutions per day: | 15.16904902 |
| mean anomaly at epoch: | 226.8635° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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