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 64962U 26145.65189042 +.00000000 +00000-0 +78449-3 0 00008
2 64962 97.3622 223.3636 0005684 277.2966 82.7634 15.40164456 01
| Epoch (UTC): | 25 May 2026 15:38:43 |
| Eccentricity: | 0.0005684 |
| inclination: | 97.3622° |
| perigee height: | 442 km |
| apogee height: | 450 km |
| right ascension of ascending node: | 223.3636° |
| argument of perigee: | 277.2966° |
| revolutions per day: | 15.40164456 |
| mean anomaly at epoch: | 82.7634° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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