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 46320U 26145.61276343 +.00000000 +00000-0 +63235-3 0 00000
2 46320 97.2481 219.1018 0001676 138.6876 221.4510 15.64844286 02
| Epoch (UTC): | 25 May 2026 14:42:22 |
| Eccentricity: | 0.0001676 |
| inclination: | 97.2481° |
| perigee height: | 373 km |
| apogee height: | 375 km |
| right ascension of ascending node: | 219.1018° |
| argument of perigee: | 138.6876° |
| revolutions per day: | 15.64844286 |
| mean anomaly at epoch: | 221.4510° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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