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 65680U 26145.27672600 +.00000000 +00000-0 +83894-3 0 00001
2 65680 53.1612 349.6290 0001397 90.9186 269.1974 15.30210903 03
| Epoch (UTC): | 25 May 2026 06:38:29 |
| Eccentricity: | 0.0001397 |
| inclination: | 53.1612° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 349.6290° |
| argument of perigee: | 90.9186° |
| revolutions per day: | 15.30210903 |
| mean anomaly at epoch: | 269.1974° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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