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 65187U 26145.40333370 +.00000000 +00000-0 +41628-3 0 00005
2 65187 97.4488 17.8902 0001941 88.4302 271.7148 15.05656717 09
| Epoch (UTC): | 25 May 2026 09:40:48 |
| Eccentricity: | 0.0001941 |
| inclination: | 97.4488° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 17.8902° |
| argument of perigee: | 88.4302° |
| revolutions per day: | 15.05656717 |
| mean anomaly at epoch: | 271.7148° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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