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 69026U 26145.58335647 +.00000000 +00000-0 -19432-1 0 00006
2 69026 97.2844 0.3372 0001693 98.0606 168.3620 15.68191667 08
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001693 |
| inclination: | 97.2844° |
| perigee height: | 363 km |
| apogee height: | 365 km |
| right ascension of ascending node: | 0.3372° |
| argument of perigee: | 98.0606° |
| revolutions per day: | 15.68191667 |
| mean anomaly at epoch: | 168.3620° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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