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 49436U 26145.60737654 +.00000000 +00000-0 +78063-3 0 00002
2 49436 53.2129 223.8241 0001506 49.2662 310.8460 15.08935637 02
| Epoch (UTC): | 25 May 2026 14:34:37 |
| Eccentricity: | 0.0001506 |
| inclination: | 53.2129° |
| perigee height: | 538 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 223.8241° |
| argument of perigee: | 49.2662° |
| revolutions per day: | 15.08935637 |
| mean anomaly at epoch: | 310.8460° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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