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 69005U 26145.25378307 +.00000000 +00000-0 +13460-3 0 00003
2 69005 97.4060 43.4801 0007054 96.5552 263.6487 15.20141641 07
| Epoch (UTC): | 25 May 2026 06:05:26 |
| Eccentricity: | 0.0007054 |
| inclination: | 97.4060° |
| perigee height: | 501 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 43.4801° |
| argument of perigee: | 96.5552° |
| revolutions per day: | 15.20141641 |
| mean anomaly at epoch: | 263.6487° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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