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 65278U 26145.42409544 +.00000000 +00000-0 +38220-3 0 00009
2 65278 97.4464 197.8694 0001006 142.8742 217.2555 15.05659606 03
| Epoch (UTC): | 25 May 2026 10:10:41 |
| Eccentricity: | 0.0001006 |
| inclination: | 97.4464° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 197.8694° |
| argument of perigee: | 142.8742° |
| revolutions per day: | 15.05659606 |
| mean anomaly at epoch: | 217.2555° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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