▸Orbital parameters

Orbit class	SSO
Inclination	97.0830°
Eccentricity	0.0006010
Period	92.3 min
Apogee	389 km
Perigee	381 km
Mean motion	15.60809885 rev/day
RAAN	265.6633°
Arg of perigee	147.2292°
Mean anomaly	212.9339°
B*	1.6037e-4
Rev at epoch	2,972

▸Two-line element set (TLE)

EPOCH Jul 7, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 67254U 25313G 26188.15141632 .00013266 00000-0 16037-3 0 9994

2 67254 97.0830 265.6633 0006010 147.2292 212.9339 15.60809885 29727

▸ source OMM (JSON)

{
  "OBJECT_NAME": "AIST-2T 2",
  "OBJECT_ID": "2025-313G",
  "EPOCH": "2026-07-07T03:38:02.37+00:00",
  "MEAN_MOTION": 15.60809885,
  "ECCENTRICITY": 0.000601,
  "INCLINATION": 97.083,
  "RA_OF_ASC_NODE": 265.6633,
  "ARG_OF_PERICENTER": 147.2292,
  "MEAN_ANOMALY": 212.9339,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 67254,
  "REV_AT_EPOCH": 2972,
  "BSTAR": 0.00016037,
  "MEAN_MOTION_DOT": 0.00013266,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	AIST-2T 2
Operator	Korporatsii RoskosmosHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Russia
Launch date	Dec 28, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	670HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/67254

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.