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 40074U 26073.91213862 +.00000000 +00000-0 +76391-3 0 00007
2 40074 98.4236 67.4061 0003289 103.5630 256.5965 15.11922479 02
| Epoch (UTC): | 14 March 2026 21:53:28 |
| Eccentricity: | 0.0003289 |
| inclination: | 98.4236° |
| perigee height: | 528 km |
| apogee height: | 533 km |
| right ascension of ascending node: | 67.4061° |
| argument of perigee: | 103.5630° |
| revolutions per day: | 15.11922479 |
| mean anomaly at epoch: | 256.5965° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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