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 62640U 26144.77800365 +.00000000 +00000-0 +27705-3 0 00008
2 62640 97.3595 226.1971 0003186 75.0345 285.1248 15.30077605 02
| Epoch (UTC): | 24 May 2026 18:40:19 |
| Eccentricity: | 0.0003186 |
| inclination: | 97.3595° |
| perigee height: | 473 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 226.1971° |
| argument of perigee: | 75.0345° |
| revolutions per day: | 15.30077605 |
| mean anomaly at epoch: | 285.1248° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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