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 65249U 26145.40000677 +.00000000 +00000-0 +38405-3 0 00004
2 65249 97.4501 188.2484 0001624 126.0691 234.0687 15.05654592 09
| Epoch (UTC): | 25 May 2026 09:36:00 |
| Eccentricity: | 0.0001624 |
| inclination: | 97.4501° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 188.2484° |
| argument of perigee: | 126.0691° |
| revolutions per day: | 15.05654592 |
| mean anomaly at epoch: | 234.0687° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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