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 48299U 26145.53053418 +.00000000 +00000-0 +26977-4 0 00007
2 48299 53.1604 77.9526 0001497 95.3481 264.7691 15.31701523 03
| Epoch (UTC): | 25 May 2026 12:43:58 |
| Eccentricity: | 0.0001497 |
| inclination: | 53.1604° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 77.9526° |
| argument of perigee: | 95.3481° |
| revolutions per day: | 15.31701523 |
| mean anomaly at epoch: | 264.7691° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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