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 21393U 26038.25562515 +.00000000 +00000-0 +52718-3 0 00007
2 21393 24.9811 162.6525 0785283 308.2898 44.9466 13.80804668 00
| Epoch (UTC): | 07 February 2026 06:08:06 |
| Eccentricity: | 0.0785283 |
| inclination: | 24.9811° |
| perigee height: | 385 km |
| apogee height: | 1537 km |
| right ascension of ascending node: | 162.6525° |
| argument of perigee: | 308.2898° |
| revolutions per day: | 13.80804668 |
| mean anomaly at epoch: | 44.9466° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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