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 28538U 26160.12323198 +.00000000 +00000-0 +91744-4 0 00002
2 28538 63.8255 307.9730 0213337 255.5882 102.1387 13.43378111 04
| Epoch (UTC): | 09 June 2026 02:57:27 |
| Eccentricity: | 0.0213337 |
| inclination: | 63.8255° |
| perigee height: | 937 km |
| apogee height: | 1256 km |
| right ascension of ascending node: | 307.9730° |
| argument of perigee: | 255.5882° |
| revolutions per day: | 13.43378111 |
| mean anomaly at epoch: | 102.1387° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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