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 48693U 26145.51187897 +.00000000 +00000-0 +50164-4 0 00007
2 48693 53.1615 77.9344 0001214 99.2002 260.9137 15.31707732 01
| Epoch (UTC): | 25 May 2026 12:17:06 |
| Eccentricity: | 0.0001214 |
| inclination: | 53.1615° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 77.9344° |
| argument of perigee: | 99.2002° |
| revolutions per day: | 15.31707732 |
| mean anomaly at epoch: | 260.9137° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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