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 49434U 26144.98732325 +.00000000 +00000-0 +24020-3 0 00004
2 49434 53.2172 246.7661 0001022 80.2175 279.8933 15.08880122 02
| Epoch (UTC): | 24 May 2026 23:41:44 |
| Eccentricity: | 0.0001022 |
| inclination: | 53.2172° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 246.7661° |
| argument of perigee: | 80.2175° |
| revolutions per day: | 15.08880122 |
| mean anomaly at epoch: | 279.8933° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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