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 02825U 26067.96395471 +.00000000 +00000-0 +99748-4 0 00006
2 02825 69.9708 288.7107 0009521 292.9835 67.0266 13.97708903 00
| Epoch (UTC): | 08 March 2026 23:08:05 |
| Eccentricity: | 0.0009521 |
| inclination: | 69.9708° |
| perigee height: | 895 km |
| apogee height: | 909 km |
| right ascension of ascending node: | 288.7107° |
| argument of perigee: | 292.9835° |
| revolutions per day: | 13.97708903 |
| mean anomaly at epoch: | 67.0266° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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