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 62269U 26145.49384451 +.00000000 +00000-0 +20566-2 0 00005
2 62269 42.9993 313.4766 0002284 268.3653 91.6953 15.70920910 09
| Epoch (UTC): | 25 May 2026 11:51:08 |
| Eccentricity: | 0.0002284 |
| inclination: | 42.9993° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 313.4766° |
| argument of perigee: | 268.3653° |
| revolutions per day: | 15.70920910 |
| mean anomaly at epoch: | 91.6953° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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