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 48294U 26145.54919108 +.00000000 +00000-0 +44678-5 0 00009
2 48294 53.1610 77.8843 0001158 77.9570 282.1561 15.31697109 09
| Epoch (UTC): | 25 May 2026 13:10:50 |
| Eccentricity: | 0.0001158 |
| inclination: | 53.1610° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 77.8843° |
| argument of perigee: | 77.9570° |
| revolutions per day: | 15.31697109 |
| mean anomaly at epoch: | 282.1561° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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