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 66996U 26145.60022198 +.00000000 +00000-0 +21375-3 0 00006
2 66996 97.6322 221.4999 0016137 81.0717 279.2335 15.05876118 08
| Epoch (UTC): | 25 May 2026 14:24:19 |
| Eccentricity: | 0.0016137 |
| inclination: | 97.6322° |
| perigee height: | 538 km |
| apogee height: | 560 km |
| right ascension of ascending node: | 221.4999° |
| argument of perigee: | 81.0717° |
| revolutions per day: | 15.05876118 |
| mean anomaly at epoch: | 279.2335° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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