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 49019U 26145.63427081 +.00000000 +00000-0 +15626-3 0 00008
2 49019 45.0038 329.2203 0006476 133.4105 226.7271 14.08547980 09
| Epoch (UTC): | 25 May 2026 15:13:20 |
| Eccentricity: | 0.0006476 |
| inclination: | 45.0038° |
| perigee height: | 860 km |
| apogee height: | 869 km |
| right ascension of ascending node: | 329.2203° |
| argument of perigee: | 133.4105° |
| revolutions per day: | 14.08547980 |
| mean anomaly at epoch: | 226.7271° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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