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 39421U 26087.87675296 +.00000000 +00000-0 +44265-3 0 00009
2 39421 97.6972 58.3939 0030064 5.5995 354.5561 15.04349008 07
| Epoch (UTC): | 28 March 2026 21:02:31 |
| Eccentricity: | 0.0030064 |
| inclination: | 97.6972° |
| perigee height: | 533 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 58.3939° |
| argument of perigee: | 5.5995° |
| revolutions per day: | 15.04349008 |
| mean anomaly at epoch: | 354.5561° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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