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 48682U 26145.20154536 +.00000000 +00000-0 +36022-4 0 00002
2 48682 53.1609 69.1452 0001175 89.1921 270.9215 15.31713926 09
| Epoch (UTC): | 25 May 2026 04:50:13 |
| Eccentricity: | 0.0001175 |
| inclination: | 53.1609° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 69.1452° |
| argument of perigee: | 89.1921° |
| revolutions per day: | 15.31713926 |
| mean anomaly at epoch: | 270.9215° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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