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 63107U 26145.41706632 +.00000000 +00000-0 +12987-2 0 00006
2 63107 43.0009 134.2717 0001383 252.4038 107.6679 15.70901122 03
| Epoch (UTC): | 25 May 2026 10:00:34 |
| Eccentricity: | 0.0001383 |
| inclination: | 43.0009° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 134.2717° |
| argument of perigee: | 252.4038° |
| revolutions per day: | 15.70901122 |
| mean anomaly at epoch: | 107.6679° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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