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 63848U 26145.33020125 +.00000000 +00000-0 +39385-3 0 00007
2 63848 42.9997 5.0497 0000375 287.2544 72.8266 15.27592842 09
| Epoch (UTC): | 25 May 2026 07:55:29 |
| Eccentricity: | 0.0000375 |
| inclination: | 42.9997° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 5.0497° |
| argument of perigee: | 287.2544° |
| revolutions per day: | 15.27592842 |
| mean anomaly at epoch: | 72.8266° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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