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 27421U 26109.08787494 +.00000000 +00000-0 +81183-4 0 00009
2 27421 97.9909 150.5555 0131052 100.2449 261.3556 14.54701506 00
| Epoch (UTC): | 19 April 2026 02:06:32 |
| Eccentricity: | 0.0131052 |
| inclination: | 97.9909° |
| perigee height: | 617 km |
| apogee height: | 803 km |
| right ascension of ascending node: | 150.5555° |
| argument of perigee: | 100.2449° |
| revolutions per day: | 14.54701506 |
| mean anomaly at epoch: | 261.3556° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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