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 26077.92094042 +.00000000 +00000-0 +00000-0 0 00000
2 23802 79.7621 228.0862 6379046 212.1493 84.5948 1.29845786 02
| Epoch (UTC): | 18 March 2026 22:06:09 |
| Eccentricity: | 0.6379046 |
| inclination: | 79.7621° |
| perigee height: | 6473 km |
| apogee height: | 51753 km |
| right ascension of ascending node: | 228.0862° |
| argument of perigee: | 212.1493° |
| revolutions per day: | 1.29845786 |
| mean anomaly at epoch: | 84.5948° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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