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 43874U 26145.79915067 +.00000000 +00000-0 +00000-0 0 00001
2 43874 2.4894 80.7527 0001354 47.2355 191.2333 1.00268510 08
| Epoch (UTC): | 25 May 2026 19:10:46 |
| Eccentricity: | 0.0001354 |
| inclination: | 2.4894° |
| perigee height: | 35782 km |
| apogee height: | 35793 km |
| right ascension of ascending node: | 80.7527° |
| argument of perigee: | 47.2355° |
| revolutions per day: | 1.00268510 |
| mean anomaly at epoch: | 191.2333° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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