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 48998U 26145.48969647 +.00000000 +00000-0 -12570-4 0 00002
2 48998 87.9105 233.2827 0001726 107.8474 252.2846 13.16596326 05
| Epoch (UTC): | 25 May 2026 11:45:09 |
| Eccentricity: | 0.0001726 |
| inclination: | 87.9105° |
| perigee height: | 1196 km |
| apogee height: | 1199 km |
| right ascension of ascending node: | 233.2827° |
| argument of perigee: | 107.8474° |
| revolutions per day: | 13.16596326 |
| mean anomaly at epoch: | 252.2846° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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