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 64074U 26145.61966856 +.00000000 +00000-0 +16029-2 0 00009
2 64074 42.9996 354.8337 0001531 262.1132 97.9562 15.70907448 05
| Epoch (UTC): | 25 May 2026 14:52:19 |
| Eccentricity: | 0.0001531 |
| inclination: | 42.9996° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 354.8337° |
| argument of perigee: | 262.1132° |
| revolutions per day: | 15.70907448 |
| mean anomaly at epoch: | 97.9562° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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