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 64441U 26145.13960904 +.00000000 +00000-0 +53505-3 0 00003
2 64441 53.1583 93.0316 0001114 97.5387 262.5743 15.34410605 02
| Epoch (UTC): | 25 May 2026 03:21:02 |
| Eccentricity: | 0.0001114 |
| inclination: | 53.1583° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 93.0316° |
| argument of perigee: | 97.5387° |
| revolutions per day: | 15.34410605 |
| mean anomaly at epoch: | 262.5743° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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