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 48474U 26145.52912712 +.00000000 +00000-0 +77366-5 0 00001
2 48474 53.1610 194.2927 0001344 103.8842 256.2309 15.30187729 07
| Epoch (UTC): | 25 May 2026 12:41:56 |
| Eccentricity: | 0.0001344 |
| inclination: | 53.1610° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 194.2927° |
| argument of perigee: | 103.8842° |
| revolutions per day: | 15.30187729 |
| mean anomaly at epoch: | 256.2309° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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