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 62660U 26145.18227178 +.00000000 +00000-0 +33368-3 0 00003
2 62660 97.3942 226.7318 0004546 71.2529 288.9204 15.29039828 00
| Epoch (UTC): | 25 May 2026 04:22:28 |
| Eccentricity: | 0.0004546 |
| inclination: | 97.3942° |
| perigee height: | 476 km |
| apogee height: | 482 km |
| right ascension of ascending node: | 226.7318° |
| argument of perigee: | 71.2529° |
| revolutions per day: | 15.29039828 |
| mean anomaly at epoch: | 288.9204° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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