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 60209U 26107.10614031 +.00000000 +00000-0 +37432-3 0 00004
2 60209 97.2386 323.4507 0012505 87.3137 272.9550 15.57252153 06
| Epoch (UTC): | 17 April 2026 02:32:50 |
| Eccentricity: | 0.0012505 |
| inclination: | 97.2386° |
| perigee height: | 387 km |
| apogee height: | 404 km |
| right ascension of ascending node: | 323.4507° |
| argument of perigee: | 87.3137° |
| revolutions per day: | 15.57252153 |
| mean anomaly at epoch: | 272.9550° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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