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 69093U 26145.60657573 +.00000000 +00000-0 +56716-3 0 00005
2 69093 97.4283 256.9710 0304029 161.3164 199.9558 15.70776132 07
| Epoch (UTC): | 25 May 2026 14:33:28 |
| Eccentricity: | 0.0304029 |
| inclination: | 97.4283° |
| perigee height: | 152 km |
| apogee height: | 561 km |
| right ascension of ascending node: | 256.9710° |
| argument of perigee: | 161.3164° |
| revolutions per day: | 15.70776132 |
| mean anomaly at epoch: | 199.9558° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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