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 39010U 26074.46712288 +.00000000 +00000-0 +91464-3 0 00000
2 39010 49.6449 251.5740 4585218 65.5257 335.0821 6.31511831 09
| Epoch (UTC): | 15 March 2026 11:12:39 |
| Eccentricity: | 0.4585218 |
| inclination: | 49.6449° |
| perigee height: | 317 km |
| apogee height: | 11655 km |
| right ascension of ascending node: | 251.5740° |
| argument of perigee: | 65.5257° |
| revolutions per day: | 6.31511831 |
| mean anomaly at epoch: | 335.0821° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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