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 25994U 26162.26133616 +.00000000 +00000-0 +71519-4 0 00004
2 25994 97.9458 212.0424 0001137 214.4897 187.4080 14.61098276 07
| Epoch (UTC): | 11 June 2026 06:16:19 |
| Eccentricity: | 0.0001137 |
| inclination: | 97.9458° |
| perigee height: | 689 km |
| apogee height: | 690 km |
| right ascension of ascending node: | 212.0424° |
| argument of perigee: | 214.4897° |
| revolutions per day: | 14.61098276 |
| mean anomaly at epoch: | 187.4080° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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