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 60603U 26145.18429444 +.00000000 +00000-0 -50670-4 0 00005
2 60603 53.1623 310.9622 0001341 107.5763 252.5386 15.34401901 07
| Epoch (UTC): | 25 May 2026 04:25:23 |
| Eccentricity: | 0.0001341 |
| inclination: | 53.1623° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 310.9622° |
| argument of perigee: | 107.5763° |
| revolutions per day: | 15.34401901 |
| mean anomaly at epoch: | 252.5386° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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