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 12149U 26121.76659287 +.00000000 +00000-0 +15657-5 0 00001
2 12149 65.8240 245.8524 0013006 197.0004 326.5396 13.72231813 00
| Epoch (UTC): | 01 May 2026 18:23:53 |
| Eccentricity: | 0.0013006 |
| inclination: | 65.8240° |
| perigee height: | 982 km |
| apogee height: | 1001 km |
| right ascension of ascending node: | 245.8524° |
| argument of perigee: | 197.0004° |
| revolutions per day: | 13.72231813 |
| mean anomaly at epoch: | 326.5396° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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