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 60298U 26145.05442699 +.00000000 +00000-0 +88284-5 0 00000
2 60298 53.1613 57.6227 0001166 92.4293 267.6842 15.31700546 05
| Epoch (UTC): | 25 May 2026 01:18:22 |
| Eccentricity: | 0.0001166 |
| inclination: | 53.1613° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 57.6227° |
| argument of perigee: | 92.4293° |
| revolutions per day: | 15.31700546 |
| mean anomaly at epoch: | 267.6842° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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