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 48681U 26145.51659102 +.00000000 +00000-0 +42351-4 0 00006
2 48681 53.1599 78.2925 0001528 91.9782 268.1395 15.31700015 03
| Epoch (UTC): | 25 May 2026 12:23:53 |
| Eccentricity: | 0.0001528 |
| inclination: | 53.1599° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 78.2925° |
| argument of perigee: | 91.9782° |
| revolutions per day: | 15.31700015 |
| mean anomaly at epoch: | 268.1395° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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