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 60348U 26145.53026825 +.00000000 +00000-0 -27171-5 0 00007
2 60348 53.1617 78.4314 0001303 89.9540 270.1611 15.31695576 01
| Epoch (UTC): | 25 May 2026 12:43:35 |
| Eccentricity: | 0.0001303 |
| inclination: | 53.1617° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 78.4314° |
| argument of perigee: | 89.9540° |
| revolutions per day: | 15.31695576 |
| mean anomaly at epoch: | 270.1611° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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