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 48485U 26145.52255130 +.00000000 +00000-0 +13435-4 0 00003
2 48485 53.1594 196.3755 0001211 91.6661 268.4479 15.31695030 01
| Epoch (UTC): | 25 May 2026 12:32:28 |
| Eccentricity: | 0.0001211 |
| inclination: | 53.1594° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 196.3755° |
| argument of perigee: | 91.6661° |
| revolutions per day: | 15.31695030 |
| mean anomaly at epoch: | 268.4479° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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