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 62963U 26145.42687038 +.00000000 +00000-0 +39078-3 0 00005
2 62963 53.1615 233.3733 0000652 131.5357 228.5701 15.34404348 02
| Epoch (UTC): | 25 May 2026 10:14:41 |
| Eccentricity: | 0.0000652 |
| inclination: | 53.1615° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 233.3733° |
| argument of perigee: | 131.5357° |
| revolutions per day: | 15.34404348 |
| mean anomaly at epoch: | 228.5701° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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