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 62948U 26145.51928169 +.00000000 +00000-0 +66204-3 0 00002
2 62948 53.1586 233.2437 0001002 93.1629 266.9487 15.30193200 02
| Epoch (UTC): | 25 May 2026 12:27:45 |
| Eccentricity: | 0.0001002 |
| inclination: | 53.1586° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 233.2437° |
| argument of perigee: | 93.1629° |
| revolutions per day: | 15.30193200 |
| mean anomaly at epoch: | 266.9487° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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