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 48999U 26145.49525514 +.00000000 +00000-0 +60398-4 0 00005
2 48999 87.9107 233.2764 0002036 102.2794 257.8565 13.16593777 03
| Epoch (UTC): | 25 May 2026 11:53:10 |
| Eccentricity: | 0.0002036 |
| inclination: | 87.9107° |
| perigee height: | 1196 km |
| apogee height: | 1199 km |
| right ascension of ascending node: | 233.2764° |
| argument of perigee: | 102.2794° |
| revolutions per day: | 13.16593777 |
| mean anomaly at epoch: | 257.8565° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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