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 26074.94884648 +.00000000 +00000-0 +60145-5 0 00004
2 07210 81.2384 159.5789 0079417 293.6634 65.6217 14.13625659 02
| Epoch (UTC): | 15 March 2026 22:46:20 |
| Eccentricity: | 0.0079417 |
| inclination: | 81.2384° |
| perigee height: | 790 km |
| apogee height: | 904 km |
| right ascension of ascending node: | 159.5789° |
| argument of perigee: | 293.6634° |
| revolutions per day: | 14.13625659 |
| mean anomaly at epoch: | 65.6217° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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