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 07369U 26104.20790999 +.00000000 +00000-0 +00000-0 0 00006
2 07369 124.8416 234.7782 0067491 69.7407 30.7122 3.07214671 02
| Epoch (UTC): | 14 April 2026 04:59:23 |
| Eccentricity: | 0.0067491 |
| inclination: | 124.8416° |
| perigee height: | 13475 km |
| apogee height: | 13745 km |
| right ascension of ascending node: | 234.7782° |
| argument of perigee: | 69.7407° |
| revolutions per day: | 3.07214671 |
| mean anomaly at epoch: | 30.7122° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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