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 48022U 26144.80397907 +.00000000 +00000-0 +10786-2 0 00003
2 48022 53.1244 332.1555 0002557 210.7828 149.3031 15.48528040 06
| Epoch (UTC): | 24 May 2026 19:17:43 |
| Eccentricity: | 0.0002557 |
| inclination: | 53.1244° |
| perigee height: | 419 km |
| apogee height: | 423 km |
| right ascension of ascending node: | 332.1555° |
| argument of perigee: | 210.7828° |
| revolutions per day: | 15.48528040 |
| mean anomaly at epoch: | 149.3031° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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