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 62261U 26142.68687727 +.00000000 +00000-0 +31146-4 0 00005
2 62261 98.1817 150.3649 0001382 90.0027 270.1331 14.59198676 06
| Epoch (UTC): | 22 May 2026 16:29:06 |
| Eccentricity: | 0.0001382 |
| inclination: | 98.1817° |
| perigee height: | 695 km |
| apogee height: | 697 km |
| right ascension of ascending node: | 150.3649° |
| argument of perigee: | 90.0027° |
| revolutions per day: | 14.59198676 |
| mean anomaly at epoch: | 270.1331° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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