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 65674U 26145.55365295 +.00000000 +00000-0 +22668-2 0 00005
2 65674 97.4460 189.5481 0002697 102.9902 257.1626 15.05710991 00
| Epoch (UTC): | 25 May 2026 13:17:15 |
| Eccentricity: | 0.0002697 |
| inclination: | 97.4460° |
| perigee height: | 547 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 189.5481° |
| argument of perigee: | 102.9902° |
| revolutions per day: | 15.05710991 |
| mean anomaly at epoch: | 257.1626° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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