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 62155U 26145.20019545 +.00000000 +00000-0 +69233-3 0 00002
2 62155 42.9993 93.5885 0001328 260.8072 99.2630 15.27594342 05
| Epoch (UTC): | 25 May 2026 04:48:16 |
| Eccentricity: | 0.0001328 |
| inclination: | 42.9993° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 93.5885° |
| argument of perigee: | 260.8072° |
| revolutions per day: | 15.27594342 |
| mean anomaly at epoch: | 99.2630° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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