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 44186U 26145.58979513 +.00000000 +00000-0 +00000-0 0 00001
2 44186 0.0502 3.5018 0001415 31.2092 91.2718 1.00282629 05
| Epoch (UTC): | 25 May 2026 14:09:18 |
| Eccentricity: | 0.0001415 |
| inclination: | 0.0502° |
| perigee height: | 35778 km |
| apogee height: | 35790 km |
| right ascension of ascending node: | 3.5018° |
| argument of perigee: | 31.2092° |
| revolutions per day: | 1.00282629 |
| mean anomaly at epoch: | 91.2718° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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