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 67777U 26145.50887198 +.00000000 +00000-0 +40565-3 0 00004
2 67777 51.8957 226.0076 0001071 61.4981 298.6089 14.79922130 02
| Epoch (UTC): | 25 May 2026 12:12:46 |
| Eccentricity: | 0.0001071 |
| inclination: | 51.8957° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 226.0076° |
| argument of perigee: | 61.4981° |
| revolutions per day: | 14.79922130 |
| mean anomaly at epoch: | 298.6089° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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