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 69049U 26145.51067808 +.00000000 +00000-0 +17905-3 0 00009
2 69049 41.4679 99.9009 0011051 279.1269 80.8319 15.59810900 08
| Epoch (UTC): | 25 May 2026 12:15:22 |
| Eccentricity: | 0.0011051 |
| inclination: | 41.4679° |
| perigee height: | 381 km |
| apogee height: | 396 km |
| right ascension of ascending node: | 99.9009° |
| argument of perigee: | 279.1269° |
| revolutions per day: | 15.59810900 |
| mean anomaly at epoch: | 80.8319° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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