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 48120U 26145.33108196 +.00000000 +00000-0 +38370-3 0 00001
2 48120 53.1588 169.3523 0002141 56.1447 303.9762 15.41396690 05
| Epoch (UTC): | 25 May 2026 07:56:45 |
| Eccentricity: | 0.0002141 |
| inclination: | 53.1588° |
| perigee height: | 441 km |
| apogee height: | 443 km |
| right ascension of ascending node: | 169.3523° |
| argument of perigee: | 56.1447° |
| revolutions per day: | 15.41396690 |
| mean anomaly at epoch: | 303.9762° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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