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 40894U 26145.59210087 +.00000000 +00000-0 +99869-4 0 00003
2 40894 97.6290 182.3123 0026537 211.4288 148.5342 14.82833983 05
| Epoch (UTC): | 25 May 2026 14:12:37 |
| Eccentricity: | 0.0026537 |
| inclination: | 97.6290° |
| perigee height: | 602 km |
| apogee height: | 639 km |
| right ascension of ascending node: | 182.3123° |
| argument of perigee: | 211.4288° |
| revolutions per day: | 14.82833983 |
| mean anomaly at epoch: | 148.5342° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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