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 26075.61026383 +.00000000 +00000-0 +00000-0 0 00007
2 23802 79.7596 228.1124 6376689 212.2273 84.4554 1.29845787 05
| Epoch (UTC): | 16 March 2026 14:38:46 |
| Eccentricity: | 0.6376689 |
| inclination: | 79.7596° |
| perigee height: | 6481 km |
| apogee height: | 51744 km |
| right ascension of ascending node: | 228.1124° |
| argument of perigee: | 212.2273° |
| revolutions per day: | 1.29845787 |
| mean anomaly at epoch: | 84.4554° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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