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 43864U 26145.52493176 +.00000000 +00000-0 +00000-0 0 00003
2 43864 0.0462 260.3823 0002796 137.4513 97.0074 1.00272802 00
| Epoch (UTC): | 25 May 2026 12:35:54 |
| Eccentricity: | 0.0002796 |
| inclination: | 0.0462° |
| perigee height: | 35775 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 260.3823° |
| argument of perigee: | 137.4513° |
| revolutions per day: | 1.00272802 |
| mean anomaly at epoch: | 97.0074° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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