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 65298U 26145.21070920 +.00000000 +00000-0 +12764-2 0 00004
2 65298 97.9641 228.8053 0017021 152.7910 207.4197 14.78840816 09
| Epoch (UTC): | 25 May 2026 05:03:25 |
| Eccentricity: | 0.0017021 |
| inclination: | 97.9641° |
| perigee height: | 621 km |
| apogee height: | 645 km |
| right ascension of ascending node: | 228.8053° |
| argument of perigee: | 152.7910° |
| revolutions per day: | 14.78840816 |
| mean anomaly at epoch: | 207.4197° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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