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 48116U 26145.44895492 +.00000000 +00000-0 +24569-4 0 00006
2 48116 53.1604 168.7237 0001467 97.7521 262.3646 15.30190882 00
| Epoch (UTC): | 25 May 2026 10:46:29 |
| Eccentricity: | 0.0001467 |
| inclination: | 53.1604° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 168.7237° |
| argument of perigee: | 97.7521° |
| revolutions per day: | 15.30190882 |
| mean anomaly at epoch: | 262.3646° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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