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 60284U 26145.01102832 +.00000000 +00000-0 +32829-4 0 00006
2 60284 53.1609 45.2913 0001301 80.8599 279.2549 15.30180857 00
| Epoch (UTC): | 25 May 2026 00:15:52 |
| Eccentricity: | 0.0001301 |
| inclination: | 53.1609° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 45.2913° |
| argument of perigee: | 80.8599° |
| revolutions per day: | 15.30180857 |
| mean anomaly at epoch: | 279.2549° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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