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 46277U 26145.64601263 +.00000000 +00000-0 +23314-3 0 00001
2 46277 97.1935 207.8331 0002714 107.5431 252.6115 15.44070201 07
| Epoch (UTC): | 25 May 2026 15:30:15 |
| Eccentricity: | 0.0002714 |
| inclination: | 97.1935° |
| perigee height: | 432 km |
| apogee height: | 436 km |
| right ascension of ascending node: | 207.8331° |
| argument of perigee: | 107.5431° |
| revolutions per day: | 15.44070201 |
| mean anomaly at epoch: | 252.6115° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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