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 60368U 26144.84694917 +.00000000 +00000-0 -25574-4 0 00009
2 60368 53.1604 316.1445 0001207 98.7986 261.3151 15.30189698 04
| Epoch (UTC): | 24 May 2026 20:19:36 |
| Eccentricity: | 0.0001207 |
| inclination: | 53.1604° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 316.1445° |
| argument of perigee: | 98.7986° |
| revolutions per day: | 15.30189698 |
| mean anomaly at epoch: | 261.3151° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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