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 48963U 26065.28371207 +.00000000 +00000-0 +73288-3 0 00003
2 48963 97.6842 252.4360 0003594 329.0208 31.0841 15.70216142 01
| Epoch (UTC): | 06 March 2026 06:48:32 |
| Eccentricity: | 0.0003594 |
| inclination: | 97.6842° |
| perigee height: | 356 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 252.4360° |
| argument of perigee: | 329.0208° |
| revolutions per day: | 15.70216142 |
| mean anomaly at epoch: | 31.0841° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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