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 62681U 26145.49373552 +.00000000 +00000-0 +40311-3 0 00004
2 62681 97.3926 227.0036 0005734 67.7556 292.4292 15.29013401 02
| Epoch (UTC): | 25 May 2026 11:50:58 |
| Eccentricity: | 0.0005734 |
| inclination: | 97.3926° |
| perigee height: | 475 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 227.0036° |
| argument of perigee: | 67.7556° |
| revolutions per day: | 15.29013401 |
| mean anomaly at epoch: | 292.4292° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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