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 48149U 26145.32303294 +.00000000 +00000-0 +69899-4 0 00008
2 48149 53.1585 156.4959 0001145 91.9358 268.1773 15.30193823 09
| Epoch (UTC): | 25 May 2026 07:45:10 |
| Eccentricity: | 0.0001145 |
| inclination: | 53.1585° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 156.4959° |
| argument of perigee: | 91.9358° |
| revolutions per day: | 15.30193823 |
| mean anomaly at epoch: | 268.1773° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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