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 43083U 26145.67449022 +.00000000 +00000-0 +18562-3 0 00008
2 43083 34.9956 287.7677 0005358 297.5188 62.4976 15.02526677 06
| Epoch (UTC): | 25 May 2026 16:11:15 |
| Eccentricity: | 0.0005358 |
| inclination: | 34.9956° |
| perigee height: | 555 km |
| apogee height: | 563 km |
| right ascension of ascending node: | 287.7677° |
| argument of perigee: | 297.5188° |
| revolutions per day: | 15.02526677 |
| mean anomaly at epoch: | 62.4976° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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