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 26072.94199269 +.00000000 +00000-0 +58700-3 0 00000
2 28738 97.3594 88.2454 0005157 35.8223 324.3379 15.60554268 02
| Epoch (UTC): | 13 March 2026 22:36:28 |
| Eccentricity: | 0.0005157 |
| inclination: | 97.3594° |
| perigee height: | 383 km |
| apogee height: | 390 km |
| right ascension of ascending node: | 88.2454° |
| argument of perigee: | 35.8223° |
| revolutions per day: | 15.60554268 |
| mean anomaly at epoch: | 324.3379° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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