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 26074.28849363 +.00000000 +00000-0 +57776-3 0 00008
2 28738 97.3594 89.6420 0004834 32.3198 327.8355 15.60699466 06
| Epoch (UTC): | 15 March 2026 06:55:25 |
| Eccentricity: | 0.0004834 |
| inclination: | 97.3594° |
| perigee height: | 382 km |
| apogee height: | 389 km |
| right ascension of ascending node: | 89.6420° |
| argument of perigee: | 32.3198° |
| revolutions per day: | 15.60699466 |
| mean anomaly at epoch: | 327.8355° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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