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 48909U 26145.06960310 +.00000000 +00000-0 +44851-3 0 00001
2 48909 97.6793 340.6744 0002064 69.0646 291.0839 15.75841241 04
| Epoch (UTC): | 25 May 2026 01:40:13 |
| Eccentricity: | 0.0002064 |
| inclination: | 97.6793° |
| perigee height: | 341 km |
| apogee height: | 344 km |
| right ascension of ascending node: | 340.6744° |
| argument of perigee: | 69.0646° |
| revolutions per day: | 15.75841241 |
| mean anomaly at epoch: | 291.0839° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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