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 65668U 26145.57304257 +.00000000 +00000-0 +85941-4 0 00006
2 65668 97.4484 189.5213 0002567 121.1111 239.0368 15.05655859 06
| Epoch (UTC): | 25 May 2026 13:45:10 |
| Eccentricity: | 0.0002567 |
| inclination: | 97.4484° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 189.5213° |
| argument of perigee: | 121.1111° |
| revolutions per day: | 15.05655859 |
| mean anomaly at epoch: | 239.0368° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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