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 62243U 26145.64952080 +.00000000 +00000-0 +12230-3 0 00003
2 62243 89.0078 18.7033 0012619 269.6558 90.3189 14.24602053 00
| Epoch (UTC): | 25 May 2026 15:35:18 |
| Eccentricity: | 0.0012619 |
| inclination: | 89.0078° |
| perigee height: | 801 km |
| apogee height: | 819 km |
| right ascension of ascending node: | 18.7033° |
| argument of perigee: | 269.6558° |
| revolutions per day: | 14.24602053 |
| mean anomaly at epoch: | 90.3189° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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