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 28738U 26069.47903596 +.00000000 +00000-0 +63901-3 0 00009
2 28738 97.3605 84.6545 0005741 44.1911 315.9803 15.60229062 01
| Epoch (UTC): | 10 March 2026 11:29:48 |
| Eccentricity: | 0.0005741 |
| inclination: | 97.3605° |
| perigee height: | 383 km |
| apogee height: | 391 km |
| right ascension of ascending node: | 84.6545° |
| argument of perigee: | 44.1911° |
| revolutions per day: | 15.60229062 |
| mean anomaly at epoch: | 315.9803° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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