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 26160.09122485 +.00000000 +00000-0 +23093-3 0 00009
2 28415 97.3375 193.2565 0030910 7.2678 352.9005 15.30506511 01
| Epoch (UTC): | 09 June 2026 02:11:21 |
| Eccentricity: | 0.0030910 |
| inclination: | 97.3375° |
| perigee height: | 453 km |
| apogee height: | 495 km |
| right ascension of ascending node: | 193.2565° |
| argument of perigee: | 7.2678° |
| revolutions per day: | 15.30506511 |
| mean anomaly at epoch: | 352.9005° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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