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 69077U 26145.60950831 +.00000000 +00000-0 +31924-4 0 00005
2 69077 88.9867 344.1981 0002803 167.3445 192.7816 14.20503106 06
| Epoch (UTC): | 25 May 2026 14:37:41 |
| Eccentricity: | 0.0002803 |
| inclination: | 88.9867° |
| perigee height: | 822 km |
| apogee height: | 826 km |
| right ascension of ascending node: | 344.1981° |
| argument of perigee: | 167.3445° |
| revolutions per day: | 14.20503106 |
| mean anomaly at epoch: | 192.7816° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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