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 27646U 26038.13685934 +.00000000 +00000-0 +39615-3 0 00003
2 27646 49.5151 286.7020 5415067 108.9812 17.4916 4.61714282 07
| Epoch (UTC): | 07 February 2026 03:17:04 |
| Eccentricity: | 0.5415067 |
| inclination: | 49.5151° |
| perigee height: | 607 km |
| apogee height: | 17105 km |
| right ascension of ascending node: | 286.7020° |
| argument of perigee: | 108.9812° |
| revolutions per day: | 4.61714282 |
| mean anomaly at epoch: | 17.4916° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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