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 48274U 26159.78589514 +.00000000 +00000-0 +27715-3 0 00003
2 48274 41.4695 13.1170 0008543 10.7662 349.3358 15.60455863 09
| Epoch (UTC): | 08 June 2026 18:51:41 |
| Eccentricity: | 0.0008543 |
| inclination: | 41.4695° |
| perigee height: | 381 km |
| apogee height: | 392 km |
| right ascension of ascending node: | 13.1170° |
| argument of perigee: | 10.7662° |
| revolutions per day: | 15.60455863 |
| mean anomaly at epoch: | 349.3358° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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