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 64192U 26145.30403104 +.00000000 +00000-0 +37210-3 0 00004
2 64192 53.1594 95.3633 0001232 79.6079 280.5061 15.30202307 01
| Epoch (UTC): | 25 May 2026 07:17:48 |
| Eccentricity: | 0.0001232 |
| inclination: | 53.1594° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 95.3633° |
| argument of perigee: | 79.6079° |
| revolutions per day: | 15.30202307 |
| mean anomaly at epoch: | 280.5061° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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