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 60289U 26145.18458172 +.00000000 +00000-0 +51971-4 0 00009
2 60289 53.1621 57.0127 0001186 94.3753 265.7384 15.31707454 06
| Epoch (UTC): | 25 May 2026 04:25:47 |
| Eccentricity: | 0.0001186 |
| inclination: | 53.1621° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 57.0127° |
| argument of perigee: | 94.3753° |
| revolutions per day: | 15.31707454 |
| mean anomaly at epoch: | 265.7384° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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