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 64425U 26145.55646417 +.00000000 +00000-0 +25400-3 0 00004
2 64425 70.0005 240.5449 0003285 262.6614 97.4172 14.98337975 04
| Epoch (UTC): | 25 May 2026 13:21:18 |
| Eccentricity: | 0.0003285 |
| inclination: | 70.0005° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 240.5449° |
| argument of perigee: | 262.6614° |
| revolutions per day: | 14.98337975 |
| mean anomaly at epoch: | 97.4172° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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