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 60404U 26145.50550302 +.00000000 +00000-0 +73210-5 0 00003
2 60404 53.1587 67.8824 0001265 88.3367 271.7796 15.69704139 03
| Epoch (UTC): | 25 May 2026 12:07:55 |
| Eccentricity: | 0.0001265 |
| inclination: | 53.1587° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 67.8824° |
| argument of perigee: | 88.3367° |
| revolutions per day: | 15.69704139 |
| mean anomaly at epoch: | 271.7796° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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