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 48127U 26145.34261604 +.00000000 +00000-0 +43447-4 0 00005
2 48127 53.1581 168.8796 0001205 82.3123 277.8015 15.31703086 03
| Epoch (UTC): | 25 May 2026 08:13:22 |
| Eccentricity: | 0.0001205 |
| inclination: | 53.1581° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 168.8796° |
| argument of perigee: | 82.3123° |
| revolutions per day: | 15.31703086 |
| mean anomaly at epoch: | 277.8015° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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