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 64294U 26145.58708118 +.00000000 +00000-0 +96469-4 0 00002
2 64294 70.0025 0.7056 0002809 267.9451 92.1386 14.98330392 03
| Epoch (UTC): | 25 May 2026 14:05:23 |
| Eccentricity: | 0.0002809 |
| inclination: | 70.0025° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 0.7056° |
| argument of perigee: | 267.9451° |
| revolutions per day: | 14.98330392 |
| mean anomaly at epoch: | 92.1386° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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