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 43890U 26145.60478692 +.00000000 +00000-0 +14018-4 0 00005
2 43890 97.4569 13.7089 0007199 228.9947 131.0655 14.98999455 05
| Epoch (UTC): | 25 May 2026 14:30:53 |
| Eccentricity: | 0.0007199 |
| inclination: | 97.4569° |
| perigee height: | 565 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 13.7089° |
| argument of perigee: | 228.9947° |
| revolutions per day: | 14.98999455 |
| mean anomaly at epoch: | 131.0655° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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