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 48683U 26145.06175714 +.00000000 +00000-0 +22819-3 0 00006
2 48683 53.1610 69.9909 0001228 86.8382 273.2760 15.31710340 09
| Epoch (UTC): | 25 May 2026 01:28:55 |
| Eccentricity: | 0.0001228 |
| inclination: | 53.1610° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 69.9909° |
| argument of perigee: | 86.8382° |
| revolutions per day: | 15.31710340 |
| mean anomaly at epoch: | 273.2760° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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