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 66295U 26145.61356878 +.00000000 +00000-0 +73147-3 0 00008
2 66295 45.3898 237.2262 0010234 310.2519 49.7474 15.26415788 04
| Epoch (UTC): | 25 May 2026 14:43:32 |
| Eccentricity: | 0.0010234 |
| inclination: | 45.3898° |
| perigee height: | 480 km |
| apogee height: | 494 km |
| right ascension of ascending node: | 237.2262° |
| argument of perigee: | 310.2519° |
| revolutions per day: | 15.26415788 |
| mean anomaly at epoch: | 49.7474° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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