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 48150U 26145.31160590 +.00000000 +00000-0 +57412-4 0 00007
2 48150 53.1587 156.3875 0001110 95.0160 265.0969 15.31710071 01
| Epoch (UTC): | 25 May 2026 07:28:42 |
| Eccentricity: | 0.0001110 |
| inclination: | 53.1587° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 156.3875° |
| argument of perigee: | 95.0160° |
| revolutions per day: | 15.31710071 |
| mean anomaly at epoch: | 265.0969° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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