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 06080U 26069.34549323 +.00000000 +00000-0 +12599-4 0 00003
2 06080 81.2422 167.7853 0048381 342.0768 17.8690 14.01290053 02
| Epoch (UTC): | 10 March 2026 08:17:30 |
| Eccentricity: | 0.0048381 |
| inclination: | 81.2422° |
| perigee height: | 854 km |
| apogee height: | 924 km |
| right ascension of ascending node: | 167.7853° |
| argument of perigee: | 342.0768° |
| revolutions per day: | 14.01290053 |
| mean anomaly at epoch: | 17.8690° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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