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 28415U 26064.98264374 +.00000000 +00000-0 +32749-3 0 00002
2 28415 97.3498 99.2692 0031378 345.0282 15.0026 15.28982464 08
| Epoch (UTC): | 05 March 2026 23:35:00 |
| Eccentricity: | 0.0031378 |
| inclination: | 97.3498° |
| perigee height: | 457 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 99.2692° |
| argument of perigee: | 345.0282° |
| revolutions per day: | 15.28982464 |
| mean anomaly at epoch: | 15.0026° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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