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 61198U 26145.60858370 +.00000000 +00000-0 +12495-3 0 00007
2 61198 44.8601 238.1264 0007857 317.7260 42.2965 13.99154804 01
| Epoch (UTC): | 25 May 2026 14:36:21 |
| Eccentricity: | 0.0007857 |
| inclination: | 44.8601° |
| perigee height: | 891 km |
| apogee height: | 902 km |
| right ascension of ascending node: | 238.1264° |
| argument of perigee: | 317.7260° |
| revolutions per day: | 13.99154804 |
| mean anomaly at epoch: | 42.2965° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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