▸Orbital parameters

Orbit class	SSO
Inclination	97.0820°
Eccentricity	0.0006410
Period	92.3 min
Apogee	390 km
Perigee	381 km
Mean motion	15.60828603 rev/day
RAAN	265.3235°
Arg of perigee	173.3715°
Mean anomaly	186.7629°
B*	1.1098e-4
Rev at epoch	2,967

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 67253U 25313F 26187.73482314 .00009153 00000-0 11098-3 0 9993

2 67253 97.0820 265.3235 0006410 173.3715 186.7629 15.60828603 29677

▸ source OMM (JSON)

{
  "OBJECT_NAME": "AIST-2T 1",
  "OBJECT_ID": "2025-313F",
  "EPOCH": "2026-07-06T17:38:08.719+00:00",
  "MEAN_MOTION": 15.60828603,
  "ECCENTRICITY": 0.000641,
  "INCLINATION": 97.082,
  "RA_OF_ASC_NODE": 265.3235,
  "ARG_OF_PERICENTER": 173.3715,
  "MEAN_ANOMALY": 186.7629,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 67253,
  "REV_AT_EPOCH": 2967,
  "BSTAR": 0.00011098,
  "MEAN_MOTION_DOT": 0.00009153,
  "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 1
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/67253

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