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 07210U 26073.60403806 +.00000000 +00000-0 +31693-4 0 00004
2 07210 81.2386 160.8965 0079428 297.5379 61.7739 14.13625647 09
| Epoch (UTC): | 14 March 2026 14:29:48 |
| Eccentricity: | 0.0079428 |
| inclination: | 81.2386° |
| perigee height: | 790 km |
| apogee height: | 904 km |
| right ascension of ascending node: | 160.8965° |
| argument of perigee: | 297.5379° |
| revolutions per day: | 14.13625647 |
| mean anomaly at epoch: | 61.7739° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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