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 62949U 26145.42268499 +.00000000 +00000-0 +42817-2 0 00009
2 62949 53.1591 233.3604 0002183 70.8844 289.2395 15.34244201 06
| Epoch (UTC): | 25 May 2026 10:08:39 |
| Eccentricity: | 0.0002183 |
| inclination: | 53.1591° |
| perigee height: | 462 km |
| apogee height: | 465 km |
| right ascension of ascending node: | 233.3604° |
| argument of perigee: | 70.8844° |
| revolutions per day: | 15.34244201 |
| mean anomaly at epoch: | 289.2395° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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