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 26155.07670466 +.00000000 +00000-0 +38850-5 0 00000
2 24278 98.5251 5.7442 0350656 130.3680 232.8639 13.53273623 01
| Epoch (UTC): | 04 June 2026 01:50:27 |
| Eccentricity: | 0.0350656 |
| inclination: | 98.5251° |
| perigee height: | 799 km |
| apogee height: | 1321 km |
| right ascension of ascending node: | 5.7442° |
| argument of perigee: | 130.3680° |
| revolutions per day: | 13.53273623 |
| mean anomaly at epoch: | 232.8639° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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