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 48398U 26145.55318531 +.00000000 +00000-0 +12833-2 0 00003
2 48398 53.0705 348.1885 0003126 29.7138 330.4034 15.19144665 02
| Epoch (UTC): | 25 May 2026 13:16:35 |
| Eccentricity: | 0.0003126 |
| inclination: | 53.0705° |
| perigee height: | 506 km |
| apogee height: | 511 km |
| right ascension of ascending node: | 348.1885° |
| argument of perigee: | 29.7138° |
| revolutions per day: | 15.19144665 |
| mean anomaly at epoch: | 330.4034° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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