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 48138U 26145.35757280 +.00000000 +00000-0 +13775-3 0 00008
2 48138 53.1579 171.1711 0000964 73.7567 286.3540 15.31720838 05
| Epoch (UTC): | 25 May 2026 08:34:54 |
| Eccentricity: | 0.0000964 |
| inclination: | 53.1579° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 171.1711° |
| argument of perigee: | 73.7567° |
| revolutions per day: | 15.31720838 |
| mean anomaly at epoch: | 286.3540° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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