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 26087.85875076 +.00000000 +00000-0 +96106-4 0 00005
2 02825 69.9703 245.9954 0009797 274.2156 85.7830 13.97713501 08
| Epoch (UTC): | 28 March 2026 20:36:36 |
| Eccentricity: | 0.0009797 |
| inclination: | 69.9703° |
| perigee height: | 895 km |
| apogee height: | 909 km |
| right ascension of ascending node: | 245.9954° |
| argument of perigee: | 274.2156° |
| revolutions per day: | 13.97713501 |
| mean anomaly at epoch: | 85.7830° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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