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 69003U 26145.00002315 +.00000000 +00000-0 +29971-2 0 00000
2 69003 97.7366 42.8821 0002190 181.5163 181.2379 14.91799615 03
| Epoch (UTC): | 25 May 2026 00:00:02 |
| Eccentricity: | 0.0002190 |
| inclination: | 97.7366° |
| perigee height: | 591 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 42.8821° |
| argument of perigee: | 181.5163° |
| revolutions per day: | 14.91799615 |
| mean anomaly at epoch: | 181.2379° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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