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 39074U 26145.48939176 +.00000000 +00000-0 +76864-4 0 00006
2 39074 51.9954 219.9079 0000198 177.5095 182.5773 12.62268183 09
| Epoch (UTC): | 25 May 2026 11:44:43 |
| Eccentricity: | 0.0000198 |
| inclination: | 51.9954° |
| perigee height: | 1413 km |
| apogee height: | 1414 km |
| right ascension of ascending node: | 219.9079° |
| argument of perigee: | 177.5095° |
| revolutions per day: | 12.62268183 |
| mean anomaly at epoch: | 182.5773° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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