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 64899U 26145.45068198 +.00000000 +00000-0 +79054-4 0 00007
2 64899 97.9833 222.9938 0015962 349.8920 10.1964 14.72297887 06
| Epoch (UTC): | 25 May 2026 10:48:58 |
| Eccentricity: | 0.0015962 |
| inclination: | 97.9833° |
| perigee height: | 643 km |
| apogee height: | 665 km |
| right ascension of ascending node: | 222.9938° |
| argument of perigee: | 349.8920° |
| revolutions per day: | 14.72297887 |
| mean anomaly at epoch: | 10.1964° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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