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 48357U 26145.33435132 +.00000000 +00000-0 +37957-4 0 00007
2 48357 53.1603 1.6878 0001204 85.5371 274.5768 15.31705508 07
| Epoch (UTC): | 25 May 2026 08:01:27 |
| Eccentricity: | 0.0001204 |
| inclination: | 53.1603° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 1.6878° |
| argument of perigee: | 85.5371° |
| revolutions per day: | 15.31705508 |
| mean anomaly at epoch: | 274.5768° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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