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 69021U 26145.65672672 +.00000000 +00000-0 +39712-3 0 00005
2 69021 97.4052 43.8540 0006634 73.7288 286.4676 15.19667187 05
| Epoch (UTC): | 25 May 2026 15:45:41 |
| Eccentricity: | 0.0006634 |
| inclination: | 97.4052° |
| perigee height: | 502 km |
| apogee height: | 511 km |
| right ascension of ascending node: | 43.8540° |
| argument of perigee: | 73.7288° |
| revolutions per day: | 15.19667187 |
| mean anomaly at epoch: | 286.4676° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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