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 49302U 26145.36741073 +.00000000 +00000-0 -84678-4 0 00008
2 49302 87.9161 309.5137 0001657 89.9132 270.2191 13.19727797 06
| Epoch (UTC): | 25 May 2026 08:49:04 |
| Eccentricity: | 0.0001657 |
| inclination: | 87.9161° |
| perigee height: | 1185 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.5137° |
| argument of perigee: | 89.9132° |
| revolutions per day: | 13.19727797 |
| mean anomaly at epoch: | 270.2191° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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