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 62272U 26145.65287044 +.00000000 +00000-0 +19850-2 0 00001
2 62272 42.9998 312.9642 0002372 251.1135 108.9476 15.71025071 05
| Epoch (UTC): | 25 May 2026 15:40:08 |
| Eccentricity: | 0.0002372 |
| inclination: | 42.9998° |
| perigee height: | 354 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 312.9642° |
| argument of perigee: | 251.1135° |
| revolutions per day: | 15.71025071 |
| mean anomaly at epoch: | 108.9476° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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