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 48678U 26145.30466683 +.00000000 +00000-0 -92778-5 0 00009
2 48678 53.1605 107.4569 0001328 86.2058 273.9095 15.31708897 04
| Epoch (UTC): | 25 May 2026 07:18:43 |
| Eccentricity: | 0.0001328 |
| inclination: | 53.1605° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 107.4569° |
| argument of perigee: | 86.2058° |
| revolutions per day: | 15.31708897 |
| mean anomaly at epoch: | 273.9095° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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