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 63948U 26145.53375991 +.00000000 +00000-0 +31450-3 0 00009
2 63948 70.0007 80.6746 0002655 270.7814 89.3040 14.98345426 04
| Epoch (UTC): | 25 May 2026 12:48:36 |
| Eccentricity: | 0.0002655 |
| inclination: | 70.0007° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 80.6746° |
| argument of perigee: | 270.7814° |
| revolutions per day: | 14.98345426 |
| mean anomaly at epoch: | 89.3040° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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