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 48859U 26137.34480044 +.00000000 +00000-0 +00000-0 0 00003
2 48859 55.1878 333.6992 0024563 229.1356 308.8651 2.00570737 05
| Epoch (UTC): | 17 May 2026 08:16:30 |
| Eccentricity: | 0.0024563 |
| inclination: | 55.1878° |
| perigee height: | 20116 km |
| apogee height: | 20247 km |
| right ascension of ascending node: | 333.6992° |
| argument of perigee: | 229.1356° |
| revolutions per day: | 2.00570737 |
| mean anomaly at epoch: | 308.8651° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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