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 27858U 26145.46796125 +.00000000 +00000-0 +62019-4 0 00003
2 27858 73.9300 216.4812 0008641 283.7890 76.2324 14.81420246 00
| Epoch (UTC): | 25 May 2026 11:13:51 |
| Eccentricity: | 0.0008641 |
| inclination: | 73.9300° |
| perigee height: | 619 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 216.4812° |
| argument of perigee: | 283.7890° |
| revolutions per day: | 14.81420246 |
| mean anomaly at epoch: | 76.2324° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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