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 63707U 26145.38757642 +.00000000 +00000-0 +75428-3 0 00005
2 63707 53.1584 223.2112 0001489 103.2217 256.8950 15.30212741 03
| Epoch (UTC): | 25 May 2026 09:18:06 |
| Eccentricity: | 0.0001489 |
| inclination: | 53.1584° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 223.2112° |
| argument of perigee: | 103.2217° |
| revolutions per day: | 15.30212741 |
| mean anomaly at epoch: | 256.8950° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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