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 64180U 26145.27872521 +.00000000 +00000-0 +10122-2 0 00002
2 64180 53.1589 95.2116 0001522 92.3263 267.7912 15.30180116 01
| Epoch (UTC): | 25 May 2026 06:41:21 |
| Eccentricity: | 0.0001522 |
| inclination: | 53.1589° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 95.2116° |
| argument of perigee: | 92.3263° |
| revolutions per day: | 15.30180116 |
| mean anomaly at epoch: | 267.7912° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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