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 60148U 26145.46236781 +.00000000 +00000-0 -72318-5 0 00004
2 60148 53.1631 313.1409 0001282 93.8868 266.2280 15.31702432 00
| Epoch (UTC): | 25 May 2026 11:05:48 |
| Eccentricity: | 0.0001282 |
| inclination: | 53.1631° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 313.1409° |
| argument of perigee: | 93.8868° |
| revolutions per day: | 15.31702432 |
| mean anomaly at epoch: | 266.2280° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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