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 60212U 26145.36404316 +.00000000 +00000-0 +21332-4 0 00004
2 60212 97.8210 153.2480 0002091 94.6410 265.5045 14.87573213 07
| Epoch (UTC): | 25 May 2026 08:44:13 |
| Eccentricity: | 0.0002091 |
| inclination: | 97.8210° |
| perigee height: | 604 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 153.2480° |
| argument of perigee: | 94.6410° |
| revolutions per day: | 14.87573213 |
| mean anomaly at epoch: | 265.5045° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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