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 63705U 26145.51187447 +.00000000 +00000-0 +25364-3 0 00002
2 63705 53.1586 222.5693 0001151 85.5020 274.6113 15.30200581 07
| Epoch (UTC): | 25 May 2026 12:17:05 |
| Eccentricity: | 0.0001151 |
| inclination: | 53.1586° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 222.5693° |
| argument of perigee: | 85.5020° |
| revolutions per day: | 15.30200581 |
| mean anomaly at epoch: | 274.6113° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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