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 62449U 26145.52539639 +.00000000 +00000-0 +48718-3 0 00009
2 62449 53.1619 338.3128 0000691 73.9588 286.1489 15.30206887 04
| Epoch (UTC): | 25 May 2026 12:36:34 |
| Eccentricity: | 0.0000691 |
| inclination: | 53.1619° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 338.3128° |
| argument of perigee: | 73.9588° |
| revolutions per day: | 15.30206887 |
| mean anomaly at epoch: | 286.1489° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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