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 51060U 26145.60277516 +.00000000 +00000-0 +27209-3 0 00000
2 51060 97.2890 211.9805 0006646 75.7286 284.4698 15.40138901 05
| Epoch (UTC): | 25 May 2026 14:27:59 |
| Eccentricity: | 0.0006646 |
| inclination: | 97.2890° |
| perigee height: | 441 km |
| apogee height: | 450 km |
| right ascension of ascending node: | 211.9805° |
| argument of perigee: | 75.7286° |
| revolutions per day: | 15.40138901 |
| mean anomaly at epoch: | 284.4698° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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