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 64120U 26145.40657314 +.00000000 +00000-0 +48291-3 0 00001
2 64120 53.1609 30.7365 0001437 87.5322 272.5843 15.30215209 04
| Epoch (UTC): | 25 May 2026 09:45:27 |
| Eccentricity: | 0.0001437 |
| inclination: | 53.1609° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 30.7365° |
| argument of perigee: | 87.5322° |
| revolutions per day: | 15.30215209 |
| mean anomaly at epoch: | 272.5843° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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