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 24278U 26138.29307405 +.00000000 +00000-0 +42085-4 0 00009
2 24278 98.5270 351.2554 0349981 173.8581 186.7023 13.53272656 05
| Epoch (UTC): | 18 May 2026 07:02:01 |
| Eccentricity: | 0.0349981 |
| inclination: | 98.5270° |
| perigee height: | 800 km |
| apogee height: | 1321 km |
| right ascension of ascending node: | 351.2554° |
| argument of perigee: | 173.8581° |
| revolutions per day: | 13.53272656 |
| mean anomaly at epoch: | 186.7023° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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