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 64012U 26145.42219284 +.00000000 +00000-0 +77718-3 0 00009
2 64012 42.9995 284.3414 0000671 292.1305 67.9476 15.27591404 02
| Epoch (UTC): | 25 May 2026 10:07:57 |
| Eccentricity: | 0.0000671 |
| inclination: | 42.9995° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 284.3414° |
| argument of perigee: | 292.1305° |
| revolutions per day: | 15.27591404 |
| mean anomaly at epoch: | 67.9476° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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