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 62661U 26145.12100014 +.00000000 +00000-0 +34894-3 0 00002
2 62661 97.4007 227.2428 0005138 62.9345 297.2419 15.29329171 07
| Epoch (UTC): | 25 May 2026 02:54:14 |
| Eccentricity: | 0.0005138 |
| inclination: | 97.4007° |
| perigee height: | 474 km |
| apogee height: | 481 km |
| right ascension of ascending node: | 227.2428° |
| argument of perigee: | 62.9345° |
| revolutions per day: | 15.29329171 |
| mean anomaly at epoch: | 297.2419° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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