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 69007U 26145.23744377 +.00000000 +00000-0 +14066-3 0 00000
2 69007 97.4068 43.5063 0009318 127.0525 233.1564 15.21287929 02
| Epoch (UTC): | 25 May 2026 05:41:55 |
| Eccentricity: | 0.0009318 |
| inclination: | 97.4068° |
| perigee height: | 496 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 43.5063° |
| argument of perigee: | 127.0525° |
| revolutions per day: | 15.21287929 |
| mean anomaly at epoch: | 233.1564° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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