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 28096U 26067.92561547 +.00000000 +00000-0 +10688-3 0 00004
2 28096 63.6792 288.2550 0073402 117.6963 243.1536 13.41063017 09
| Epoch (UTC): | 08 March 2026 22:12:53 |
| Eccentricity: | 0.0073402 |
| inclination: | 63.6792° |
| perigee height: | 1050 km |
| apogee height: | 1160 km |
| right ascension of ascending node: | 288.2550° |
| argument of perigee: | 117.6963° |
| revolutions per day: | 13.41063017 |
| mean anomaly at epoch: | 243.1536° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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