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 54361U 26145.62008016 +.00000000 +00000-0 +78475-4 0 00008
2 54361 98.3524 244.1153 0002118 75.6572 284.4855 14.46984433 08
| Epoch (UTC): | 25 May 2026 14:52:54 |
| Eccentricity: | 0.0002118 |
| inclination: | 98.3524° |
| perigee height: | 734 km |
| apogee height: | 737 km |
| right ascension of ascending node: | 244.1153° |
| argument of perigee: | 75.6572° |
| revolutions per day: | 14.46984433 |
| mean anomaly at epoch: | 284.4855° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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