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 69004U 26145.25563529 +.00000000 +00000-0 +13302-3 0 00009
2 69004 97.4072 43.4854 0006149 92.8721 267.3218 15.20010212 00
| Epoch (UTC): | 25 May 2026 06:08:06 |
| Eccentricity: | 0.0006149 |
| inclination: | 97.4072° |
| perigee height: | 502 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 43.4854° |
| argument of perigee: | 92.8721° |
| revolutions per day: | 15.20010212 |
| mean anomaly at epoch: | 267.3218° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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