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 65667U 26145.57581054 +.00000000 +00000-0 +15863-3 0 00002
2 65667 97.4491 189.5173 0002270 117.7717 242.3740 15.05655875 01
| Epoch (UTC): | 25 May 2026 13:49:10 |
| Eccentricity: | 0.0002270 |
| inclination: | 97.4491° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 189.5173° |
| argument of perigee: | 117.7717° |
| revolutions per day: | 15.05655875 |
| mean anomaly at epoch: | 242.3740° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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