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 67095U 26145.36803162 +.00000000 +00000-0 +32628-3 0 00001
2 67095 70.0011 181.0961 0004751 265.5955 94.4662 14.98333840 02
| Epoch (UTC): | 25 May 2026 08:49:57 |
| Eccentricity: | 0.0004751 |
| inclination: | 70.0011° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 181.0961° |
| argument of perigee: | 265.5955° |
| revolutions per day: | 14.98333840 |
| mean anomaly at epoch: | 94.4662° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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