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 62118U 26145.45623852 +.00000000 +00000-0 +65698-3 0 00001
2 62118 42.9988 62.2842 0000457 163.6317 196.4550 15.27596652 05
| Epoch (UTC): | 25 May 2026 10:56:59 |
| Eccentricity: | 0.0000457 |
| inclination: | 42.9988° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 62.2842° |
| argument of perigee: | 163.6317° |
| revolutions per day: | 15.27596652 |
| mean anomaly at epoch: | 196.4550° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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