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 64730U 26145.50071877 +.00000000 +00000-0 +76695-3 0 00002
2 64730 53.1596 184.1456 0001663 57.9138 302.2024 15.30192686 03
| Epoch (UTC): | 25 May 2026 12:01:02 |
| Eccentricity: | 0.0001663 |
| inclination: | 53.1596° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.1456° |
| argument of perigee: | 57.9138° |
| revolutions per day: | 15.30192686 |
| mean anomaly at epoch: | 302.2024° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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