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 60290U 26145.06000683 +.00000000 +00000-0 +41176-4 0 00004
2 60290 53.1604 57.6539 0001143 93.7241 266.3890 15.30193635 08
| Epoch (UTC): | 25 May 2026 01:26:24 |
| Eccentricity: | 0.0001143 |
| inclination: | 53.1604° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 57.6539° |
| argument of perigee: | 93.7241° |
| revolutions per day: | 15.30193635 |
| mean anomaly at epoch: | 266.3890° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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