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 63843U 26145.31220700 +.00000000 +00000-0 +75521-3 0 00003
2 63843 43.0023 4.9110 0001044 279.1238 80.9495 15.27590391 01
| Epoch (UTC): | 25 May 2026 07:29:34 |
| Eccentricity: | 0.0001044 |
| inclination: | 43.0023° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 4.9110° |
| argument of perigee: | 279.1238° |
| revolutions per day: | 15.27590391 |
| mean anomaly at epoch: | 80.9495° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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