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 49293U 26145.66340888 +.00000000 +00000-0 -22214-3 0 00006
2 49293 87.9179 278.9307 0001714 102.2686 257.8639 13.20772029 07
| Epoch (UTC): | 25 May 2026 15:55:18 |
| Eccentricity: | 0.0001714 |
| inclination: | 87.9179° |
| perigee height: | 1180 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 278.9307° |
| argument of perigee: | 102.2686° |
| revolutions per day: | 13.20772029 |
| mean anomaly at epoch: | 257.8639° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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