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 02828U 26087.81221311 +.00000000 +00000-0 +90256-4 0 00001
2 02828 69.9701 235.5906 0010489 271.9884 88.0021 13.98069555 05
| Epoch (UTC): | 28 March 2026 19:29:35 |
| Eccentricity: | 0.0010489 |
| inclination: | 69.9701° |
| perigee height: | 893 km |
| apogee height: | 908 km |
| right ascension of ascending node: | 235.5906° |
| argument of perigee: | 271.9884° |
| revolutions per day: | 13.98069555 |
| mean anomaly at epoch: | 88.0021° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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