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 23802U 26027.85666934 +.00000000 +00000-0 +00000-0 0 00002
2 23802 79.6890 228.6446 6328535 213.8256 81.7411 1.29845981 06
| Epoch (UTC): | 27 January 2026 20:33:36 |
| Eccentricity: | 0.6328535 |
| inclination: | 79.6890° |
| perigee height: | 6652 km |
| apogee height: | 51573 km |
| right ascension of ascending node: | 228.6446° |
| argument of perigee: | 213.8256° |
| revolutions per day: | 1.29845981 |
| mean anomaly at epoch: | 81.7411° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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