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 63933U 26145.51705836 +.00000000 +00000-0 +28934-3 0 00009
2 63933 70.0012 80.6115 0002916 268.2169 91.8656 14.98341691 00
| Epoch (UTC): | 25 May 2026 12:24:33 |
| Eccentricity: | 0.0002916 |
| inclination: | 70.0012° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 80.6115° |
| argument of perigee: | 268.2169° |
| revolutions per day: | 14.98341691 |
| mean anomaly at epoch: | 91.8656° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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