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 60297U 26145.17524663 +.00000000 +00000-0 +40422-4 0 00005
2 60297 53.1611 56.9521 0001188 83.9394 276.1742 15.31708673 05
| Epoch (UTC): | 25 May 2026 04:12:21 |
| Eccentricity: | 0.0001188 |
| inclination: | 53.1611° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 56.9521° |
| argument of perigee: | 83.9394° |
| revolutions per day: | 15.31708673 |
| mean anomaly at epoch: | 276.1742° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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