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 23439U 26098.22898661 +.00000000 +00000-0 +85260-4 0 00006
2 23439 64.8176 56.3548 0153793 16.5628 344.0242 11.27583810 07
| Epoch (UTC): | 08 April 2026 05:29:44 |
| Eccentricity: | 0.0153793 |
| inclination: | 64.8176° |
| perigee height: | 1893 km |
| apogee height: | 2152 km |
| right ascension of ascending node: | 56.3548° |
| argument of perigee: | 16.5628° |
| revolutions per day: | 11.27583810 |
| mean anomaly at epoch: | 344.0242° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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