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 62849U 26145.05573521 +.00000000 +00000-0 +59368-3 0 00002
2 62849 43.0007 17.4004 0001292 268.5557 91.5147 15.27603046 04
| Epoch (UTC): | 25 May 2026 01:20:15 |
| Eccentricity: | 0.0001292 |
| inclination: | 43.0007° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 17.4004° |
| argument of perigee: | 268.5557° |
| revolutions per day: | 15.27603046 |
| mean anomaly at epoch: | 91.5147° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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