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 49289U 26145.66426616 +.00000000 +00000-0 -33948-2 0 00000
2 49289 87.9159 278.9254 0004175 92.0804 268.0808 13.20736980 01
| Epoch (UTC): | 25 May 2026 15:56:32 |
| Eccentricity: | 0.0004175 |
| inclination: | 87.9159° |
| perigee height: | 1179 km |
| apogee height: | 1185 km |
| right ascension of ascending node: | 278.9254° |
| argument of perigee: | 92.0804° |
| revolutions per day: | 13.20736980 |
| mean anomaly at epoch: | 268.0808° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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