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 24819U 26121.47292514 +.00000000 +00000-0 +00000-0 0 00003
2 24819 11.4419 38.1143 0010166 43.8354 119.6436 0.99504192 06
| Epoch (UTC): | 01 May 2026 11:21:00 |
| Eccentricity: | 0.0010166 |
| inclination: | 11.4419° |
| perigee height: | 35960 km |
| apogee height: | 36046 km |
| right ascension of ascending node: | 38.1143° |
| argument of perigee: | 43.8354° |
| revolutions per day: | 0.99504192 |
| mean anomaly at epoch: | 119.6436° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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