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 64945U 26145.56335100 +.00000000 +00000-0 +16791-3 0 00009
2 64945 97.4489 9.4821 0002416 87.9328 272.2175 15.05653568 05
| Epoch (UTC): | 25 May 2026 13:31:13 |
| Eccentricity: | 0.0002416 |
| inclination: | 97.4489° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 9.4821° |
| argument of perigee: | 87.9328° |
| revolutions per day: | 15.05653568 |
| mean anomaly at epoch: | 272.2175° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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