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 65671U 26145.36259112 +.00000000 +00000-0 +34550-3 0 00005
2 65671 97.4454 189.3435 0001006 126.3626 233.7694 15.05658352 00
| Epoch (UTC): | 25 May 2026 08:42:07 |
| Eccentricity: | 0.0001006 |
| inclination: | 97.4454° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 189.3435° |
| argument of perigee: | 126.3626° |
| revolutions per day: | 15.05658352 |
| mean anomaly at epoch: | 233.7694° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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