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 60597U 26145.48054507 +.00000000 +00000-0 +20193-4 0 00000
2 60597 53.1617 310.6781 0001067 105.4594 254.6525 15.30198239 00
| Epoch (UTC): | 25 May 2026 11:31:59 |
| Eccentricity: | 0.0001067 |
| inclination: | 53.1617° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 310.6781° |
| argument of perigee: | 105.4594° |
| revolutions per day: | 15.30198239 |
| mean anomaly at epoch: | 254.6525° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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